CYGFM04, 41885
Orbit data source: Space-Track
CYGFM04, 41885 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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41885 intel report (Beta)
CYGFM04 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 6 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 6 hours ago
0 CYGFM04
1 41885U 16078B 24361.53518287 .00023207 00000-0 65616-3 0 9994
2 41885 34.9357 139.2513 0008460 171.3426 188.7438 15.35360868445675Epoch: 2024-12-26T12:50Z
Definitive object data (Epoch: 2024-12-26T12:50:39.799Z)
| Latitude | -0.00006° |
| Longitude | -148.9278° |
| Altitude | 464.46 km |
| Speed | 7.633 km/s |
| True Right ascension | 09h 17m 00s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -4.18292° |
| Longitude | -156.56377° |
| Altitude | 465.125 km |
| Speed | 7.633 km/s |
| Apparent Right ascension | 07h 48m 05s |
| Apparent Declination | -22° 11' 52" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 18:25:53 |
| Azimuth | 309.356° NW |
| Elevation | -65.146° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 468.914 km |
| Perigee altitude | 457.339 km |
| Semi-major axis | 6,841.264 km |
| Eccentricity | 0.000846 |
| Inclination | 34.9357° |
| RAAN | 139.2513° |
| Arg. of periapsis | 171.3426° |
| True anomaly | 188.72908° |
| Mean anomaly | 188.7438° |
| Eccentric anomaly | 188.73644° |
| Mean motion | 3.83565 °/min |
| BSTAR | 0.00065616 |
| Orbital period | 93.86 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 |
CYGFM04 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-27 14:06:17.767Z | 219.48° SW | 2024-12-27 14:08:17.767Z | 172.521° S | 25.931° | 2024-12-27 14:11:17.767Z | 109.529° ESE |
| 5 mins | 2024-12-27 15:45:17.767Z | 235.212° WSW | 2024-12-27 15:47:17.767Z | 173.339° S | 29.836° | 2024-12-27 15:50:17.767Z | 116.948° SE |
Authenticating...
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