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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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: 23 hours ago
TLE from 23 hours ago
0 CYGFM05
1 41884U 16078A 26256.76401196 .00025628 00000-0 29992-3 0 9999
2 41884 34.9571 32.3593 0005582 281.3032 78.7066 15.60523325542580Epoch: 2026-09-13T18:20Z
TLE epoch observation values (Epoch: 2026-09-13T18:20:10.633Z)
Latitude
-0.00003°
Longitude
124.56097°
Altitude
384.292 km
Speed
7.682 km/s
True Right ascension
02h 09m 26s
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
09:57:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
393.232 km
Perigee altitude
385.677 km
Semi-major axis
6,767.591 km
Eccentricity
0.00056
Inclination
34.9571°
RAAN
32.3593°
Arg. of periapsis
281.3032°
True anomaly
78.76934°
Mean anomaly
78.7066°
Eccentric anomaly
78.73797°
Mean motion
3.89845 °/min
Orbital period
92.34 mins
BSTAR
0.00029992
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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 | 2026-09-15 13:37:58.127Z | 211.138° SW | 2026-09-15 13:38:58.127Z | 182.941° SSW | 26.771° | 2026-09-15 13:41:58.127Z | 110.893° ESE |
| 4 mins | 2026-09-15 15:14:58.127Z | 229.034° WSW | 2026-09-15 15:15:58.127Z | 198.278° SSW | 30.441° | 2026-09-15 15:18:58.127Z | 122.425° SE |
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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