CYGFM02, 41886
Orbit data source: Space-Track
CYGFM02, 41886 is an American payload satellite in LEO that was launched on Thu, 15 Dec 2016 UTC via a PEGASUS XL launch vehicle from the Pegasus Launch, Eastern Range Air Space (ERAS). 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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41886 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SST-US
Mission
Extended mission Civil Earth Obs Sci
Bus & Motor
CYGNSS, Unknown motor
Mass
29 kg wet, 29 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Half Hex Cyl + 2 Pan, 2.5 m
Radar Cross Section
0.450 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 CYGFM02
1 41886U 16078C 26315.16909453 .00091245 00000-0 46082-3 0 9997
2 41886 34.9387 308.8487 0007865 194.6263 165.4241 15.80271151552295Epoch: 2026-11-11T04:03Z
TLE epoch observation values (Epoch: 2026-11-11T04:03:29.767Z)
Latitude
-0.00005°
Longitude
-162.3462°
Altitude
333.651 km
Speed
7.708 km/s
True Right ascension
20h 35m 23s
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
12:21:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
338.292 km
Perigee altitude
327.736 km
Semi-major axis
6,711.151 km
Eccentricity
0.00079
Inclination
34.9387°
RAAN
308.8487°
Arg. of periapsis
194.6263°
True anomaly
165.44676°
Mean anomaly
165.4241°
Eccentric anomaly
165.43543°
Mean motion
3.94773 °/min
Orbital period
91.19 mins
BSTAR
0.00046082
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Other satellites on launch #78 in the year 2016 (2016-12-15 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.CYGFM02 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 | 2026-11-12 04:36:41.490Z | 220.239° SW | 2026-11-12 04:38:41.490Z | 164.076° S | 23.625° | 2026-11-12 04:40:41.490Z | 115.828° SE |
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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