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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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: 18 hours ago
TLE from 18 hours ago
0 IRIDIUM 118
1 42807U 17039E 26082.35873681 .00000157 00000-0 49112-4 0 9994
2 42807 86.3999 29.4905 0002149 83.8265 276.3176 14.34218780457640Epoch: 2026-03-23T08:36Z
TLE epoch observation values (Epoch: 2026-03-23T08:36:34.860Z)
Latitude
0.00003°
Longitude
79.49337°
Altitude
780.546 km
Speed
7.464 km/s
True Right ascension
01h 57m 57s
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
08:01:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.165 km
Perigee altitude
773.091 km
Semi-major axis
7,152.765 km
Eccentricity
0.00021
Inclination
86.3999°
RAAN
29.4905°
Arg. of periapsis
83.8265°
True anomaly
276.29312°
Mean anomaly
276.3176°
Eccentric anomaly
276.30536°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000049112
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-03-24 08:38:36.425Z | 354.451° N | 2026-03-24 08:42:36.425Z | 207.949° SW | 43.704° | 2026-03-24 08:46:36.425Z | 182.988° SSW |
| 6 mins | 2026-03-24 19:55:36.425Z | 114.519° SE | 2026-03-24 19:57:36.425Z | 83.353° E | 21.633° | 2026-03-24 20:01:36.425Z | 31.39° NE |
| 8 mins | 2026-03-24 21:34:36.425Z | 217.966° SW | 2026-03-24 21:38:36.425Z | 290.144° WNW | 30.767° | 2026-03-24 21:42:36.425Z | 343.957° 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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