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, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 IRIDIUM 118
1 42807U 17039E 25310.12406256 .00000029 00000-0 31901-5 0 9998
2 42807 86.3941 86.8868 0002139 90.2787 269.8654 14.34217456437973Epoch: 2025-11-06T02:58Z
TLE epoch observation values (Epoch: 2025-11-06T02:58:39.005Z)
Latitude
0°
Longitude
-3.36261°
Altitude
780.723 km
Speed
7.463 km/s
True Right ascension
05h 47m 32s
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
10:53:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.163 km
Perigee altitude
773.103 km
Semi-major axis
7,152.77 km
Eccentricity
0.00021
Inclination
86.3941°
RAAN
86.8868°
Arg. of periapsis
90.2787°
True anomaly
269.84089°
Mean anomaly
269.8654°
Eccentric anomaly
269.85314°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.0000031901
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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 | 2025-11-06 20:18:27.726Z | 32.518° NE | 2025-11-06 20:21:27.726Z | 70.484° E | 19.389° | 2025-11-06 20:25:27.726Z | 123.296° SE |
| 8 mins | 2025-11-06 21:59:27.726Z | 335.114° NNW | 2025-11-06 22:02:27.726Z | 283.513° WNW | 33.721° | 2025-11-06 22:07:27.726Z | 204.801° SW |
| 8 mins | 2025-11-07 09:14:27.726Z | 151.514° SSE | 2025-11-07 09:18:27.726Z | 78.192° E | 34.372° | 2025-11-07 09:22:27.726Z | 18.822° NNE |
| 6 mins | 2025-11-07 10:56:27.726Z | 246.168° WSW | 2025-11-07 10:59:27.726Z | 288.399° WNW | 19.011° | 2025-11-07 11:02:27.726Z | 326.511° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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