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IRIDIUM 102, 41920

Orbit data source: Space-Track

IRIDIUM 102, 41920 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
41920, 2017-003D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
2017-01-14 (10 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 IRIDIUM 102
1 41920U 17003D   26230.08164584  .00000013  00000-0 -24876-5 0  9993
2 41920  86.3914  62.5439 0002162  87.3866 272.7577 14.34217715502152
Epoch: 2026-08-18T01:57Z
TLE epoch observation values (Epoch: 2026-08-18T01:57:34.200Z)
Latitude
-0.00005°
Longitude
66.69682°
Altitude
780.644 km
Speed
7.464 km/s
True Right ascension
04h 10m 10s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
08:05:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.178 km
Perigee altitude
773.085 km
Semi-major axis
7,152.769 km
Eccentricity
0.00022
Inclination
86.3914°
RAAN
62.5439°
Arg. of periapsis
87.3866°
True anomaly
272.73295°
Mean anomaly
272.7577°
Eccentric anomaly
272.74533°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000024876
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