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: 9 hours ago
TLE from 9 hours ago
0 IRIDIUM 115
1 42806U 17039D 25342.66675462 .00000734 00000-0 21209-3 0 9999
2 42806 86.4504 41.7079 0002307 108.7126 251.4325 14.43282413446787Epoch: 2025-12-08T16:00Z
TLE epoch observation values (Epoch: 2025-12-08T16:00:07.599Z)
Latitude
-0.00005°
Longitude
84.01373°
Altitude
751.262 km
Speed
7.479 km/s
True Right ascension
02h 46m 49s
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
23:21:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.268 km
Perigee altitude
742.981 km
Semi-major axis
7,122.762 km
Eccentricity
0.00023
Inclination
86.4504°
RAAN
41.7079°
Arg. of periapsis
108.7126°
True anomaly
251.40744°
Mean anomaly
251.4325°
Eccentric anomaly
251.41997°
Mean motion
3.61053 °/min
Orbital period
99.71 mins
BSTAR
0.00021209
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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 | 2025-12-09 03:46:21.906Z | 135.204° SSE | 2025-12-09 03:50:21.906Z | 79.245° E | 23.153° | 2025-12-09 03:53:21.906Z | 35.408° NE |
| 7 mins | 2025-12-09 05:27:21.906Z | 229.082° WSW | 2025-12-09 05:30:21.906Z | 285.387° WNW | 28.097° | 2025-12-09 05:34:21.906Z | 341.161° N |
| 8 mins | 2025-12-09 15:53:21.906Z | 14.741° NNE | 2025-12-09 15:56:21.906Z | 76.481° E | 38.708° | 2025-12-09 16:01:21.906Z | 161.879° S |
| 4 mins | 2025-12-09 17:34:21.906Z | 304.238° NW | 2025-12-09 17:36:21.906Z | 277.419° WNW | 15.054° | 2025-12-09 17:38:21.906Z | 251.937° W |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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