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: 2 days ago
TLE from 2 days ago
0 IRIDIUM 115
1 42806U 17039D 26171.44645499 .00000260 00000-0 71235-4 0 9992
2 42806 86.4499 320.7270 0002005 92.4155 267.7275 14.43277662474739Epoch: 2026-06-20T10:42Z
TLE epoch observation values (Epoch: 2026-06-20T10:42:53.711Z)
Latitude
-0.00005°
Longitude
-108.65776°
Altitude
750.811 km
Speed
7.479 km/s
True Right ascension
21h 22m 54s
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
23:21:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.068 km
Perigee altitude
743.212 km
Semi-major axis
7,122.777 km
Eccentricity
0.0002
Inclination
86.4499°
RAAN
320.727°
Arg. of periapsis
92.4155°
True anomaly
267.70454°
Mean anomaly
267.7275°
Eccentric anomaly
267.71602°
Mean motion
3.61051 °/min
Orbital period
99.71 mins
BSTAR
0.000071235
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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 | 2026-06-22 21:31:51.653Z | 12.854° NNE | 2026-06-22 21:35:51.653Z | 84.227° E | 36.66° | 2026-06-22 21:39:51.653Z | 155.145° SSE |
| 4 mins | 2026-06-22 23:13:51.653Z | 303.331° NW | 2026-06-22 23:15:51.653Z | 274.811° WNW | 16.517° | 2026-06-22 23:17:51.653Z | 248.522° W |
| 8 mins | 2026-06-23 10:23:51.653Z | 184.651° SSW | 2026-06-23 10:26:51.653Z | 249.059° W | 44.836° | 2026-06-23 10:31:51.653Z | 1.105° NNE |
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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