CYGFM07, 41890
Orbit data source: Space-Track
CYGFM07, 41890 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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41890 intel report (Beta)
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Edit Public Description
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: 21 hours ago
TLE from 21 hours ago
0 CYGFM07
1 41890U 16078G 25286.76133866 .00025134 00000-0 48603-3 0 9996
2 41890 34.9482 53.7177 0009218 17.6025 342.5014 15.46740727490651Epoch: 2025-10-13T18:16Z
TLE epoch observation values (Epoch: 2025-10-13T18:16:19.660Z)
Latitude
-0.00002°
Longitude
117.07627°
Altitude
419.178 km
Speed
7.665 km/s
True Right ascension
03h 34m 52s
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
10:00:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
435.835 km
Perigee altitude
423.285 km
Semi-major axis
6,807.697 km
Eccentricity
0.00092
Inclination
34.9482°
RAAN
53.7177°
Arg. of periapsis
17.6025°
True anomaly
342.4696°
Mean anomaly
342.5014°
Eccentric anomaly
342.48551°
Mean motion
3.86405 °/min
Orbital period
93.17 mins
BSTAR
0.00048603
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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.CYGFM07 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 | 2025-10-14 16:24:10.981Z | 237.065° WSW | 2025-10-14 16:26:10.981Z | 190.991° SSW | 20.174° | 2025-10-14 16:28:10.981Z | 149.775° SSE |
| 4 mins | 2025-10-15 12:22:10.981Z | 197.448° SSW | 2025-10-15 12:23:10.981Z | 174.347° S | 19.675° | 2025-10-15 12:26:10.981Z | 112.479° ESE |
| 4 mins | 2025-10-15 14:00:10.981Z | 220.426° SW | 2025-10-15 14:01:10.981Z | 186.966° SSW | 29.075° | 2025-10-15 14:04:10.981Z | 114.234° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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