IRIDIUM 118, 42807
Orbit data source: Space-Track
IRIDIUM 118, 42807 is a payload satellite owned by Iridium (US) in LEO that was launched on Sun, 25 Jun 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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42807 intel report (Beta)
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Edit Public Description
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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 IRIDIUM 118
1 42807U 17039E 25259.05350590 .00000045 00000-0 89038-5 0 9993
2 42807 86.3926 108.2587 0001947 91.5594 268.5825 14.34217784430657Epoch: 2025-09-16T01:17Z
TLE epoch observation values (Epoch: 2025-09-16T01:17:02.909Z)
Latitude
-0.00002°
Longitude
93.74725°
Altitude
780.753 km
Speed
7.463 km/s
True Right ascension
07h 13m 02s
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
10:22:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.024 km
Perigee altitude
773.239 km
Semi-major axis
7,152.769 km
Eccentricity
0.00019
Inclination
86.3926°
RAAN
108.2587°
Arg. of periapsis
91.5594°
True anomaly
268.5602°
Mean anomaly
268.5825°
Eccentric anomaly
268.57135°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.0000089038
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Other satellites on launch #39 in the year 2017 (2017-06-25 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 118 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-17 01:18:48.430Z | 27.28° NE | 2025-09-17 01:22:48.430Z | 89.924° E | 25.137° | 2025-09-17 01:25:48.430Z | 132.171° SE |
| 7 mins | 2025-09-17 02:59:48.430Z | 326.834° NNW | 2025-09-17 03:02:48.430Z | 279.724° WNW | 26.895° | 2025-09-17 03:06:48.430Z | 220.108° SW |
| 8 mins | 2025-09-17 14:14:48.430Z | 164.123° S | 2025-09-17 14:18:48.430Z | 67.55° E | 40.768° | 2025-09-17 14:22:48.430Z | 11.387° NNE |
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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