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, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 IRIDIUM 115
1 42806U 17039D 25259.53908661 .00000133 00000-0 33481-4 0 9991
2 42806 86.4438 76.4623 0002878 92.2470 267.9060 14.43279440434797Epoch: 2025-09-16T12:56Z
TLE epoch observation values (Epoch: 2025-09-16T12:56:17.083Z)
Latitude
-0.00005°
Longitude
-113.33682°
Altitude
750.824 km
Speed
7.479 km/s
True Right ascension
05h 05m 50s
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
22:07:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.684 km
Perigee altitude
742.585 km
Semi-major axis
7,122.771 km
Eccentricity
0.00029
Inclination
86.4438°
RAAN
76.4623°
Arg. of periapsis
92.247°
True anomaly
267.87304°
Mean anomaly
267.906°
Eccentric anomaly
267.88952°
Mean motion
3.61052 °/min
Orbital period
99.71 mins
BSTAR
0.000033481
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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 | 2025-09-17 12:20:58.226Z | 176.754° S | 2025-09-17 12:24:58.226Z | 108.172° ESE | 44.642° | 2025-09-17 12:29:58.226Z | 4.555° NNE |
| 6 mins | 2025-09-17 22:47:58.226Z | 34.423° NE | 2025-09-17 22:50:58.226Z | 71.809° E | 17.134° | 2025-09-17 22:53:58.226Z | 112.555° SE |
| 8 mins | 2025-09-18 00:27:58.226Z | 340.184° N | 2025-09-18 00:31:58.226Z | 259.373° W | 35.584° | 2025-09-18 00:35:58.226Z | 202.201° 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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