IRIDIUM 115, 42806
Orbit data source: Space-Track
IRIDIUM 115, 42806 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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42806 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 115
1 42806U 17039D 25298.43368113 .00000294 00000-0 81257-4 0 9997
2 42806 86.4493 60.1905 0001863 80.9655 279.1757 14.43281897440405Epoch: 2025-10-25T10:24Z
TLE epoch observation values (Epoch: 2025-10-25T10:24:30.049Z)
Latitude
-0°
Longitude
-129.999°
Altitude
750.529 km
Speed
7.479 km/s
True Right ascension
04h 00m 45s
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
17:24:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
745.953 km
Perigee altitude
743.299 km
Semi-major axis
7,122.763 km
Eccentricity
0.00019
Inclination
86.4493°
RAAN
60.1905°
Arg. of periapsis
80.9655°
True anomaly
279.15462°
Mean anomaly
279.1757°
Eccentric anomaly
279.16516°
Mean motion
3.61053 °/min
Orbital period
99.71 mins
BSTAR
0.000081257
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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 115 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 | 2025-10-26 08:09:14.888Z | 149.808° SSE | 2025-10-26 08:13:14.888Z | 92.075° ESE | 30.983° | 2025-10-26 08:17:14.888Z | 23.903° NE |
| 6 mins | 2025-10-26 09:51:14.888Z | 244.92° WSW | 2025-10-26 09:53:14.888Z | 274.631° WNW | 20.629° | 2025-10-26 09:57:14.888Z | 330.485° NNW |
| 8 mins | 2025-10-26 20:16:14.888Z | 1.064° NNE | 2025-10-26 20:20:14.888Z | 130.314° SE | 44.297° | 2025-10-26 20:24:14.888Z | 174.597° S |
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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