CYGFM05, 41884
Orbit data source: Space-Track
CYGFM05, 41884 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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41884 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: 15 hours ago
TLE from 15 hours ago
0 CYGFM05
1 41884U 16078A 25338.67495588 .00035272 00000-0 67027-3 0 9994
2 41884 34.9586 99.7926 0009404 106.2136 253.9621 15.47189275498514Epoch: 2025-12-04T16:11Z
TLE epoch observation values (Epoch: 2025-12-04T16:11:56.188Z)
Latitude
0.00002°
Longitude
143.0805°
Altitude
425.617 km
Speed
7.657 km/s
True Right ascension
06h 39m 10s
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
04:42:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.645 km
Perigee altitude
421.843 km
Semi-major axis
6,806.381 km
Eccentricity
0.00094
Inclination
34.9586°
RAAN
99.7926°
Arg. of periapsis
106.2136°
True anomaly
253.85857°
Mean anomaly
253.9621°
Eccentric anomaly
253.91033°
Mean motion
3.86517 °/min
Orbital period
93.14 mins
BSTAR
0.00067027
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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.CYGFM05 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 | 2025-12-05 12:36:07.241Z | 209.403° SW | 2025-12-05 12:38:07.241Z | 163.36° S | 21.103° | 2025-12-05 12:40:07.241Z | 118.94° SE |
| 4 mins | 2025-12-05 14:14:07.241Z | 232.376° WSW | 2025-12-05 14:16:07.241Z | 168.63° S | 28.894° | 2025-12-05 14:18:07.241Z | 120.291° SE |
| 4 mins | 2025-12-05 15:52:07.241Z | 232.826° WSW | 2025-12-05 15:54:07.241Z | 181.222° SSW | 20.786° | 2025-12-05 15:56:07.241Z | 142.997° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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