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: 2 days ago
TLE from 2 days ago
0 CYGFM05
1 41884U 16078A 26171.32171544 .00019452 00000-0 26251-3 0 9991
2 41884 34.9559 239.8312 0007362 181.9302 178.1395 15.56789762529244Epoch: 2026-06-20T07:43Z
TLE epoch observation values (Epoch: 2026-06-20T07:43:16.214Z)
Latitude
0.00001°
Longitude
-144.52436°
Altitude
400.825 km
Speed
7.67 km/s
True Right ascension
15h 59m 19s
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
21:38:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
405.25 km
Perigee altitude
395.27 km
Semi-major axis
6,778.397 km
Eccentricity
0.00074
Inclination
34.9559°
RAAN
239.8312°
Arg. of periapsis
181.9302°
True anomaly
178.14224°
Mean anomaly
178.1395°
Eccentric anomaly
178.14087°
Mean motion
3.88913 °/min
Orbital period
92.57 mins
BSTAR
0.00026251
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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 | 2026-06-22 10:54:11.991Z | 241.837° WSW | 2026-06-22 10:56:11.991Z | 190.538° SSW | 25.565° | 2026-06-22 10:58:11.991Z | 136.472° SSE |
| 4 mins | 2026-06-23 08:21:11.991Z | 212.789° SW | 2026-06-23 08:23:11.991Z | 154.339° SSE | 23.361° | 2026-06-23 08:25:11.991Z | 113.389° SE |
| 4 mins | 2026-06-23 09:58:11.991Z | 236.231° WSW | 2026-06-23 10:00:11.991Z | 174.362° S | 27.351° | 2026-06-23 10:02:11.991Z | 125.908° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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