132
ago to ensure that ships could stay in constant touch
by telephone via GEO satellites.
Over the years Inmarsat has continued to intro-
duce new technologies and services, particularly to
the maritime community: Inmarsat-A, -B, -C, -M,
Mini-M, GAN, -D/D+, MPDS and the Fleet family
(Fleet77, 55 and 33), based on older technologies
termed "Existing and Evolved", mostly providing
fax/data services with rates up to 9.6 kbps and medi-
um/’high’ speed data up to 128 kbps.
Recently Inmarsat introduced the novel BGAN
concept, which benefits from the new I-4 satellites to
offer a shared-channel IP packet-switched service of
up to 492 kbps, and a streaming-IP service from 32
to 256 kbps. The BGAN family includes Fleet
Broadband, a service planned for ships and the mari-
time community.
Another GEO-based alternative is represented by
the various VSAT systems, utilizing satellite stations
with typically dish antennas smaller than 3 m in di-
ameter (most VSAT antenna diameters ranging from
75 cm to 1.2 m) to obtain data rates generally from
narrowband up to 4 Mbps (46 Mbps being presently
the fastest one [7]).
DVB-RCS represents a novel broadband VSAT-
type multi-user design included in the Digital Video
Broadcasting (DVB) family, and thus being the only
open international standard for satellite networks
with two-way communications, providing high ca-
pacity towards the user (∼40 Mbps downlink) and
more moderate capacity from the user (∼2 Mbps up-
link). DVB-RCS technology allows for star and
mesh topologies with 10.000's of VSATs per net-
work. Over 100 DVB-RCS systems are operating
worldwide today - going mobile with handover from
satellite to satellite, and numerous trials including
train-, aircraft- and vessel-mounted terminals.
The only seemingly interesting LEO alternative is
the Iridium constellation, using 66 cross-linked sat-
ellites in near polar orbit inclined 86.4° to the equa-
tor at an altitude of 780 km - and accordingly an or-
bit period of about 100 minutes - providing allegedly
‘true’ global coverage.
The nominal data rate of an Iridium ‘channel’ is
4.7 kbps, with latency for data connections about 1.8
s (round-trip) using small packets [8]. Iridium is also
advertising a "Direct Internet" at 10 kbps, but this
throughput is seemingly attainable only with com-
pressible data subjected to Iridium's proprietary (re-
mote) compression software.
The recent service offered by Iridium is Open-
Port, claiming IP-based data rates of 9.6 -128 kbps
(configurable), featuring allegedly global gap-free,
pole-to-pole coverage, with low-profile omnidirec-
tional antennas independent of stabilization plat-
forms.
Iridium is also planning a new generation of sat-
ellites - ‘Iridium NEXT’, to be operational by 2016,
and expected to provide date speeds up to 1 Mbps
(transportable K
a
-band up to 10 Mbps (?)) [9].
Contrary to GEOs and LEOs the HEOs are char-
acterized by a relatively low-altitude perigee and a
high-altitude apogee. These elongated orbits have
the advantage of long dwell times near a point in the
sky during the approach to and descent from apogee
- a phenomenon known as the ‘apogee dwell’ in ac-
cordance with Kepler’s second law. The orbital ec-
centricity is adjusted to the rotation of the Earth in
order to make the satellites operating near the apo-
gee and moving with nearly the same speed as the
Earth, thereby maintaining a fixed position in rela-
tion to a point on the ground.
During the early 1960's Soviet Union aerospace
engineers devised the Molniya HEO, which is simu-
lating the convenience of a GEO while simultane-
ously servicing the extreme northern regions, with
an inclination of (ideally) 63.45° relative to the
Earth’s equatorial plane, and an orbital period of ½ a
sidereal day. During this orbital period the Earth
makes ½ a turn, and thus the apogeum will be at the
very same position relative to earth twice a day.
Seen from the Earth a Molniya orbit satellite will
thus apparently be in zenith about 39.750 km above
two positions (at latitude 63.45°- see Figure 5) dur-
ing roughly 8 hours twice each day, the perigee
height being only about 500 km. Accordingly 2 sat-
ellites would provide continuous coverage of the
northern hemisphere, but a 3-satellite constellation is
preferable [10].
Apart from the evident Russian applications, sev-
eral studies on utilizing Molniya orbits for quite a
few applications have been carried out, recognizing
their apparent benefits in:
− Providing a quasi-stationary perspective with an
apogee height approximating the GEO, and thus
GEO technologies can be reused (slightly modi-
fied) to a.o. reduce costs and risks
− Giving an optimum high-latitude coverage per
satellite with no LEO-like latitudinal coverage
gaps, and little time “wasted” over lower latitudes
adequately seen from GEOs
− Simple ground segment; real-time communi-
cations can be achieved with a single primary
ground station, as for GEO
− More cost-effective than GEO systems for the de-
livery of satellite-based mobile multimedia in Eu-
rope [10].