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: 5 hours ago
TLE from 5 hours ago
0 IRIDIUM 115
1 42806U 17039D 26262.89382785 .00000072 00000-0 15482-4 0 9991
2 42806 86.4445 282.5010 0002292 86.3139 273.8324 14.43279606487927Epoch: 2026-09-19T21:27Z
TLE epoch observation values (Epoch: 2026-09-19T21:27:06.726Z)
Latitude
-0.00001°
Longitude
-38.07285°
Altitude
750.639 km
Speed
7.479 km/s
True Right ascension
18h 50m 00s
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
19:05:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.266 km
Perigee altitude
743.001 km
Semi-major axis
7,122.771 km
Eccentricity
0.00023
Inclination
86.4445°
RAAN
282.501°
Arg. of periapsis
86.3139°
True anomaly
273.80619°
Mean anomaly
273.8324°
Eccentric anomaly
273.8193°
Mean motion
3.61052 °/min
Orbital period
99.71 mins
BSTAR
0.000015482
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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 | 2026-09-20 02:33:24.745Z | 206.768° SW | 2026-09-20 02:37:24.745Z | 264.372° W | 42.627° | 2026-09-20 02:42:24.745Z | 347.985° N |
| 7 mins | 2026-09-20 13:01:24.745Z | 25.124° NE | 2026-09-20 13:04:24.745Z | 86.341° E | 39.876° | 2026-09-20 13:08:24.745Z | 149.194° SSE |
| 6 mins | 2026-09-20 14:41:24.745Z | 316.64° NNW | 2026-09-20 14:44:24.745Z | 272.956° WNW | 20.761° | 2026-09-20 14:47:24.745Z | 234.279° WSW |
| 9 mins | 2026-09-21 01:51:24.745Z | 176.306° S | 2026-09-21 01:55:24.745Z | 80.346° E | 80.606° | 2026-09-21 02:00:24.745Z | 4.65° 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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