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 26035.48869050 .00000461 00000-0 13094-3 0 9997
2 42806 86.4504 17.5276 0002302 76.9672 283.1786 14.43278897455126Epoch: 2026-02-04T11:43Z
TLE epoch observation values (Epoch: 2026-02-04T11:43:42.859Z)
Latitude
0.00001°
Longitude
66.94448°
Altitude
750.376 km
Speed
7.48 km/s
True Right ascension
01h 10m 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
18:29:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.276 km
Perigee altitude
742.996 km
Semi-major axis
7,122.773 km
Eccentricity
0.00023
Inclination
86.4504°
RAAN
17.5276°
Arg. of periapsis
76.9672°
True anomaly
283.15291°
Mean anomaly
283.1786°
Eccentric anomaly
283.16576°
Mean motion
3.61052 °/min
Orbital period
99.71 mins
BSTAR
0.00013094
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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 | 2026-02-04 23:30:08.852Z | 193.704° SSW | 2026-02-04 23:34:08.852Z | 309.778° NW | 41.792° | 2026-02-04 23:38:08.852Z | 356.133° N |
| 7 mins | 2026-02-05 09:57:08.852Z | 33.543° NE | 2026-02-05 10:00:08.852Z | 81.322° E | 23.784° | 2026-02-05 10:04:08.852Z | 135.419° SSE |
| 7 mins | 2026-02-05 11:37:08.852Z | 326.506° NNW | 2026-02-05 11:40:08.852Z | 274.918° WNW | 27.597° | 2026-02-05 11:44:08.852Z | 216.639° SW |
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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