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: 15 hours ago
TLE from 15 hours ago
0 IRIDIUM 115
1 42806U 17039D 26082.49499214 .00000417 00000-0 11786-3 0 9998
2 42806 86.4557 357.8997 0002025 94.9782 265.1650 14.43279836461905Epoch: 2026-03-23T11:52Z
TLE epoch observation values (Epoch: 2026-03-23T11:52:47.320Z)
Latitude
-0.00006°
Longitude
-1.28365°
Altitude
750.869 km
Speed
7.479 km/s
True Right ascension
23h 51m 35s
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
08:02:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.075 km
Perigee altitude
743.191 km
Semi-major axis
7,122.77 km
Eccentricity
0.0002
Inclination
86.4557°
RAAN
357.8997°
Arg. of periapsis
94.9782°
True anomaly
265.14188°
Mean anomaly
265.165°
Eccentric anomaly
265.15344°
Mean motion
3.61052 °/min
Orbital period
99.71 mins
BSTAR
0.00011786
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-24 05:07:15.349Z | 49.18° ENE | 2026-03-24 05:09:15.349Z | 74.374° E | 13.828° | 2026-03-24 05:11:15.349Z | 99.646° ESE |
| 8 mins | 2026-03-24 06:46:15.349Z | 345.77° N | 2026-03-24 06:50:15.349Z | 244.328° WSW | 39.907° | 2026-03-24 06:54:15.349Z | 193.627° SSW |
| 6 mins | 2026-03-24 17:58:15.349Z | 128.493° SE | 2026-03-24 18:01:15.349Z | 78.518° E | 24.68° | 2026-03-24 18:04:15.349Z | 33.636° NE |
| 7 mins | 2026-03-24 19:38:15.349Z | 231.898° WSW | 2026-03-24 19:41:15.349Z | 285.435° WNW | 26.423° | 2026-03-24 19:45:15.349Z | 339.82° N |
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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