IRIDIUM 104, 41922
Orbit data source: Space-Track
IRIDIUM 104, 41922 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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41922 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 IRIDIUM 104
1 41922U 17003F 26305.23502545 .00000075 00000-0 19802-4 0 9997
2 41922 86.4003 31.1616 0001987 90.1900 269.9523 14.34218022512914Epoch: 2026-11-01T05:38Z
TLE epoch observation values (Epoch: 2026-11-01T05:38:26.198Z)
Latitude
-0.0001°
Longitude
-93.97688°
Altitude
780.719 km
Speed
7.463 km/s
True Right ascension
02h 04m 38s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:44:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.052 km
Perigee altitude
773.209 km
Semi-major axis
7,152.768 km
Eccentricity
0.0002
Inclination
86.4003°
RAAN
31.1616°
Arg. of periapsis
90.19°
True anomaly
269.92953°
Mean anomaly
269.9523°
Eccentric anomaly
269.94092°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000019802
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 104 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-11-01 17:55:38.719Z | 0.581° NNE | 2026-11-01 18:00:38.719Z | 74.571° E | 76.961° | 2026-11-01 18:05:38.719Z | 173.447° S |
| 5 mins | 2026-11-02 05:14:38.719Z | 103.745° ESE | 2026-11-02 05:16:38.719Z | 75.722° E | 18.097° | 2026-11-02 05:19:38.719Z | 39.487° NE |
| 9 mins | 2026-11-02 06:52:38.719Z | 205.33° SW | 2026-11-02 06:56:38.719Z | 276.152° WNW | 48.908° | 2026-11-02 07:01:38.719Z | 351.031° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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