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 | 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 CYGFM02
1 41886U 16078C 24339.92095156 .00022707 00000-0 64394-3 0 9994
2 41886 34.9469 279.5016 0012702 317.4289 42.5444 15.35227057442448Epoch: 2024-12-04T22:06Z
Definitive object data (Epoch: 2024-12-04T22:06:10.214Z)
| Latitude | 0.00001° |
| Longitude | -126.25012° |
| Altitude | 452.749 km |
| Speed | 7.647 km/s |
| True Right ascension | 18h 38m 00s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -1.10363° |
| Longitude | -129.4865° |
| Altitude | 452.443 km |
| Speed | 7.647 km/s |
| Apparent Right ascension | 16h 43m 52s |
| Apparent Declination | -22° 34' 08" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 02:17:37 |
| Azimuth | 288.265° WNW |
| Elevation | -54.601° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 472.212 km |
| Perigee altitude | 454.832 km |
| Semi-major axis | 6,841.659 km |
| Eccentricity | 0.0012702 |
| Inclination | 34.9469° |
| RAAN | 279.5016° |
| Arg. of periapsis | 317.4289° |
| True anomaly | 42.64293° |
| Mean anomaly | 42.5444° |
| Eccentric anomaly | 42.59366° |
| Mean motion | 3.83531 °/min |
| BSTAR | 0.00064394 |
| 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 |
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 | 2024-12-05 04:49:14.186Z | 232.651° WSW | 2024-12-05 04:51:14.186Z | 191.906° SSW | 17.503° | 2024-12-05 04:53:14.186Z | 157.275° SSE |
| 4 mins | 2024-12-06 00:56:14.186Z | 214.546° SW | 2024-12-06 00:58:14.186Z | 158.582° S | 26.313° | 2024-12-06 01:00:14.186Z | 115.214° SE |
| 5 mins | 2024-12-06 02:34:14.186Z | 243.332° WSW | 2024-12-06 02:36:14.186Z | 197.612° SSW | 29.655° | 2024-12-06 02:39:14.186Z | 122.369° SE |
Authenticating...
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