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 25310.28925501 .00000053 00000-0 98894-5 0 9994
2 42806 86.4510 55.2363 0001465 92.1472 267.9897 14.43278677442110Epoch: 2025-11-06T06:56Z
TLE epoch observation values (Epoch: 2025-11-06T06:56:31.632Z)
Latitude
-0.00001°
Longitude
-94.64521°
Altitude
750.788 km
Speed
7.479 km/s
True Right ascension
03h 40m 56s
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
15:42:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
745.68 km
Perigee altitude
743.593 km
Semi-major axis
7,122.774 km
Eccentricity
0.00015
Inclination
86.451°
RAAN
55.2363°
Arg. of periapsis
92.1472°
True anomaly
267.97292°
Mean anomaly
267.9897°
Eccentric anomaly
267.98131°
Mean motion
3.61052 °/min
Orbital period
99.71 mins
BSTAR
0.0000098894
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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 | 2025-11-07 08:01:50.659Z | 202.41° SSW | 2025-11-07 08:04:50.659Z | 257.101° W | 39.193° | 2025-11-07 08:09:50.659Z | 352.733° N |
| 7 mins | 2025-11-07 18:28:50.659Z | 31.477° NE | 2025-11-07 18:31:50.659Z | 85.57° E | 27.31° | 2025-11-07 18:35:50.659Z | 141.664° SSE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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