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: 7 hours ago
TLE from 7 hours ago
0 IRIDIUM 115
1 42806U 17039D 26038.05393019 .00000559 00000-0 16020-3 0 9990
2 42806 86.4508 16.4554 0002231 76.5464 283.5986 14.43282021455493Epoch: 2026-02-07T01:17Z
TLE epoch observation values (Epoch: 2026-02-07T01:17:39.568Z)
Latitude
0.00004°
Longitude
-140.14243°
Altitude
750.366 km
Speed
7.48 km/s
True Right ascension
01h 05m 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
10:52:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.215 km
Perigee altitude
743.037 km
Semi-major axis
7,122.763 km
Eccentricity
0.00022
Inclination
86.4508°
RAAN
16.4554°
Arg. of periapsis
76.5464°
True anomaly
283.57375°
Mean anomaly
283.5986°
Eccentric anomaly
283.58618°
Mean motion
3.61053 °/min
Orbital period
99.71 mins
BSTAR
0.0001602
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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 | 2026-02-07 10:11:28.236Z | 13.022° NNE | 2026-02-07 10:15:28.236Z | 82.125° E | 36.247° | 2026-02-07 10:19:28.236Z | 154.2° SSE |
| 4 mins | 2026-02-07 11:53:28.236Z | 304.227° NW | 2026-02-07 11:55:28.236Z | 275.559° WNW | 16.841° | 2026-02-07 11:57:28.236Z | 248.796° W |
| 8 mins | 2026-02-07 23:03:28.236Z | 183.65° SSW | 2026-02-07 23:06:28.236Z | 226.362° WSW | 44.849° | 2026-02-07 23:11:28.236Z | 1.444° NNE |
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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