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: 13 hours ago
TLE from 13 hours ago
0 CYGFM05
1 41884U 16078A 25291.72940518 .00028988 00000-0 60113-3 0 9991
2 41884 34.9605 45.7000 0009480 31.3538 328.7747 15.44686971491243Epoch: 2025-10-18T17:30Z
TLE epoch observation values (Epoch: 2025-10-18T17:30:20.607Z)
Latitude
0°
Longitude
115.6579°
Altitude
425.673 km
Speed
7.661 km/s
True Right ascension
03h 02m 48s
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
01:27:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
442.045 km
Perigee altitude
429.126 km
Semi-major axis
6,813.722 km
Eccentricity
0.00095
Inclination
34.9605°
RAAN
45.7°
Arg. of periapsis
31.3538°
True anomaly
328.71833°
Mean anomaly
328.7747°
Eccentric anomaly
328.74652°
Mean motion
3.85893 °/min
Orbital period
93.29 mins
BSTAR
0.00060113
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-19 12:23:33.619Z | 223.734° SW | 2025-10-19 12:26:33.619Z | 156.821° SSE | 23.36° | 2025-10-19 12:28:33.619Z | 114.84° SE |
| 4 mins | 2025-10-19 14:02:33.619Z | 233.199° WSW | 2025-10-19 14:04:33.619Z | 167.931° S | 28.775° | 2025-10-19 14:06:33.619Z | 122.401° SE |
| 4 mins | 2025-10-19 15:40:33.619Z | 233.033° WSW | 2025-10-19 15:42:33.619Z | 186.548° SSW | 19.004° | 2025-10-19 15:44:33.619Z | 149.492° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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