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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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: 6 hours ago
TLE from 6 hours ago
0 IRIDIUM 115
1 42806U 17039D 26128.11467744 .00000262 00000-0 72012-4 0 9999
2 42806 86.4503 338.8473 0002372 83.9189 276.2282 14.43278522468483Epoch: 2026-05-08T02:45Z
TLE epoch observation values (Epoch: 2026-05-08T02:45:08.130Z)
Latitude
-0.00006°
Longitude
71.61232°
Altitude
750.568 km
Speed
7.479 km/s
True Right ascension
22h 35m 23s
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
16:42:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.327 km
Perigee altitude
742.948 km
Semi-major axis
7,122.774 km
Eccentricity
0.00024
Inclination
86.4503°
RAAN
338.8473°
Arg. of periapsis
83.9189°
True anomaly
276.20118°
Mean anomaly
276.2282°
Eccentric anomaly
276.21469°
Mean motion
3.61052 °/min
Orbital period
99.71 mins
BSTAR
0.000072012
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-08 14:30:49.436Z | 175.678° S | 2026-05-08 14:34:49.436Z | 124.719° SE | 44.222° | 2026-05-08 14:39:49.436Z | 5.227° NNE |
| 4 mins | 2026-05-09 00:59:49.436Z | 55.599° ENE | 2026-05-09 01:00:49.436Z | 69.761° E | 16.594° | 2026-05-09 01:03:49.436Z | 110.465° ESE |
| 8 mins | 2026-05-09 02:37:49.436Z | 341.715° N | 2026-05-09 02:41:49.436Z | 264.187° W | 36.531° | 2026-05-09 02:45:49.436Z | 201.735° SSW |
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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