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: 13 hours ago
TLE from 13 hours ago
0 IRIDIUM 115
1 42806U 17039D 25293.44186721 .00000864 00000-0 25091-3 0 9992
2 42806 86.4487 62.2773 0001969 75.8482 284.2938 14.43282482439689Epoch: 2025-10-20T10:36Z
TLE epoch observation values (Epoch: 2025-10-20T10:36:17.326Z)
Latitude
-0.00001°
Longitude
-125.93902°
Altitude
750.392 km
Speed
7.48 km/s
True Right ascension
04h 09m 06s
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
18:18:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.027 km
Perigee altitude
743.222 km
Semi-major axis
7,122.761 km
Eccentricity
0.0002
Inclination
86.4487°
RAAN
62.2773°
Arg. of periapsis
75.8482°
True anomaly
284.27193°
Mean anomaly
284.2938°
Eccentric anomaly
284.28287°
Mean motion
3.61053 °/min
Orbital period
99.71 mins
BSTAR
0.00025091
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-21 08:22:08.945Z | 130.983° SE | 2025-10-21 08:25:08.945Z | 86.988° E | 23.603° | 2025-10-21 08:29:08.945Z | 30.002° NE |
| 7 mins | 2025-10-21 10:02:08.945Z | 225.988° WSW | 2025-10-21 10:05:08.945Z | 275.897° WNW | 27.651° | 2025-10-21 10:09:08.945Z | 338.087° N |
| 8 mins | 2025-10-21 20:28:08.945Z | 11.779° NNE | 2025-10-21 20:32:08.945Z | 105.496° ESE | 38.703° | 2025-10-21 20:36:08.945Z | 161.504° 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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