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). Payloads include a variety of satellites, spacecraft, and rockets 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)
CYGFM02 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 22 hours ago |
| Origin | |
| Manufacturer | SST-US |
| Mission | Extended mission Civil Science |
| Bus & Motor | CYGNSS, Unknown motor |
| Mass | 29 kg wet, 29 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Half Hex Cyl + 2 Pan, 1.7 m |
| Radar Cross Section | 0.450 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 22 hours ago
0 CYGFM02
1 41886U 16078C 24360.85442533 .00023611 00000-0 65221-3 0 9990
2 41886 34.9445 145.1944 0010701 157.5841 202.5346 15.36062536445660Epoch: 2024-12-25T20:30Z
Definitive object data (Epoch: 2024-12-25T20:30:22.348Z)
| Latitude | -0.00001° |
| Longitude | 102.75907° |
| Altitude | 463.417 km |
| Speed | 7.633 km/s |
| True Right ascension | 09h 40m 46s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 26.3083° |
| Longitude | -127.95082° |
| Altitude | 450.921 km |
| Speed | 7.65 km/s |
| Apparent Right ascension | 18h 22m 13s |
| Apparent Declination | -40° 51' 23" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 18:16:51 |
| Azimuth | 178.972° S |
| Elevation | 9.218° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 468.362 km |
| Perigee altitude | 453.725 km |
| Semi-major axis | 6,839.181 km |
| Eccentricity | 0.0010701 |
| Inclination | 34.9445° |
| RAAN | 145.1944° |
| Arg. of periapsis | 157.5841° |
| True anomaly | 202.48766° |
| Mean anomaly | 202.5346° |
| Eccentric anomaly | 202.51113° |
| Mean motion | 3.8374 °/min |
| BSTAR | 0.00065221 |
| Orbital period | 93.81 mins |
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Other satellites on launch #78 in the year 2016 (2016-12-15 UTC)
| CYGFM05, 41884 |
| CYGFM04, 41885 |
| CYGFM02, 41886 |
| CYGFM01, 41887 |
| CYGFM08, 41888 |
| CYGFM06, 41889 (Decayed) |
| CYGFM07, 41890 |
| CYGFM03, 41891 |
| PEGASUS R/B, 41892 |
CYGFM02 Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-27 13:18:17.226Z | 204.646° SW | 2024-12-27 13:20:17.226Z | 168.779° S | 18.191° | 2024-12-27 13:22:17.226Z | 126.604° SE |
| 5 mins | 2024-12-27 14:57:17.226Z | 227.861° WSW | 2024-12-27 14:59:17.226Z | 168.521° S | 29.708° | 2024-12-27 15:02:17.226Z | 109.414° ESE |
| 4 mins | 2024-12-27 16:36:17.226Z | 230.777° WSW | 2024-12-27 16:37:17.226Z | 204.366° SW | 25.811° | 2024-12-27 16:40:17.226Z | 133.305° SE |
Authenticating...
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