Showing default

CYGFM01, 41887

Orbit data source: Space-Track

CYGFM01, 41887 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.

Loading next visibility...
Identifier
41887, 2016-078D
Orbit
LEO
Country
Flag of USUS
Related 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)
2016-12-15 (9 years ago)
Launch vehicle
PEGASUS XL
Launch site
Pegasus Launch, Eastern Range Air Space (ERAS)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 CYGFM01
1 41887U 16078D   26082.22689657  .00027322  00000-0  41759-3 0  9998
2 41887  34.9401 109.9005 0005272  47.0542 313.0623 15.53382836515310
Epoch: 2026-03-23T05:26Z
TLE epoch observation values (Epoch: 2026-03-23T05:26:43.863Z)
Latitude
-0.00001°
Longitude
-152.50421°
Altitude
403.303 km
Speed
7.672 km/s
True Right ascension
07h 19m 36s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:45:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
413.739 km
Perigee altitude
406.582 km
Semi-major axis
6,788.297 km
Eccentricity
0.00053
Inclination
34.9401°
RAAN
109.9005°
Arg. of periapsis
47.0542°
True anomaly
313.01814°
Mean anomaly
313.0623°
Eccentric anomaly
313.04022°
Mean motion
3.88063 °/min
Orbital period
92.77 mins
BSTAR
0.00041759
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|