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: 13 hours ago
TLE from 13 hours ago
0 IRIDIUM 115
1 42806U 17039D 26125.34144525 .00000342 00000-0 95710-4 0 9999
2 42806 86.4503 340.0066 0002440 83.9977 276.1502 14.43281838468081Epoch: 2026-05-05T08:11Z
TLE epoch observation values (Epoch: 2026-05-05T08:11:40.869Z)
Latitude
-0.00002°
Longitude
-6.13137°
Altitude
750.554 km
Speed
7.479 km/s
True Right ascension
22h 40m 01s
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
05:02:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.364 km
Perigee altitude
742.888 km
Semi-major axis
7,122.763 km
Eccentricity
0.00024
Inclination
86.4503°
RAAN
340.0066°
Arg. of periapsis
83.9977°
True anomaly
276.1224°
Mean anomaly
276.1502°
Eccentric anomaly
276.1363°
Mean motion
3.61053 °/min
Orbital period
99.71 mins
BSTAR
0.00009571
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-06 01:24:44.593Z | 29.086° NE | 2026-05-06 01:28:44.593Z | 83.639° E | 20.324° | 2026-05-06 01:31:44.593Z | 123.904° SE |
| 7 mins | 2026-05-06 03:05:44.593Z | 329.655° NNW | 2026-05-06 03:08:44.593Z | 270.456° WNW | 31.552° | 2026-05-06 03:12:44.593Z | 210.007° SW |
| 7 mins | 2026-05-06 14:16:44.593Z | 146.896° SSE | 2026-05-06 14:19:44.593Z | 89.024° E | 33.88° | 2026-05-06 14:23:44.593Z | 20.385° NNE |
| 5 mins | 2026-05-06 15:57:44.593Z | 248.983° W | 2026-05-06 15:59:44.593Z | 277.265° WNW | 18.584° | 2026-05-06 16:02:44.593Z | 320.118° NNW |
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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