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: 5 hours ago
TLE from 5 hours ago
0 IRIDIUM 115
1 42806U 17039D 25340.65616117 .00000728 00000-0 21046-3 0 9990
2 42806 86.4508 42.5483 0002234 109.3644 250.7799 14.43279683446490Epoch: 2025-12-06T15:44Z
TLE epoch observation values (Epoch: 2025-12-06T15:44:52.325Z)
Latitude
0.00004°
Longitude
90.64951°
Altitude
751.272 km
Speed
7.479 km/s
True Right ascension
02h 50m 11s
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
19:01:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.225 km
Perigee altitude
743.042 km
Semi-major axis
7,122.771 km
Eccentricity
0.00022
Inclination
86.4508°
RAAN
42.5483°
Arg. of periapsis
109.3644°
True anomaly
250.75573°
Mean anomaly
250.7799°
Eccentric anomaly
250.76781°
Mean motion
3.61052 °/min
Orbital period
99.71 mins
BSTAR
0.00021046
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-07 03:33:20.177Z | 101.416° ESE | 2025-12-07 03:35:20.177Z | 76.09° E | 13.656° | 2025-12-07 03:37:20.177Z | 51.508° ENE |
| 8 mins | 2025-12-07 05:11:20.177Z | 199.764° SSW | 2025-12-07 05:14:20.177Z | 254.902° W | 40.381° | 2025-12-07 05:19:20.177Z | 354.009° N |
| 7 mins | 2025-12-07 15:38:20.177Z | 32.971° NE | 2025-12-07 15:41:20.177Z | 85.53° E | 26.032° | 2025-12-07 15:45:20.177Z | 139.969° SSE |
| 6 mins | 2025-12-07 17:18:20.177Z | 322.043° NNW | 2025-12-07 17:21:20.177Z | 271.163° WNW | 25.043° | 2025-12-07 17:24:20.177Z | 226.231° WSW |
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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