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 Science
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, 0.8 m
Radar Cross Section
0.450 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 CYGFM05
1 41884U 16078A 25259.33401238 .00017064 00000-0 37366-3 0 9990
2 41884 34.9594 256.1355 0007729 93.1987 266.9618 15.43178558486238Epoch: 2025-09-16T08:00Z
TLE epoch observation values (Epoch: 2025-09-16T08:00:58.669Z)
Latitude
0°
Longitude
140.36524°
Altitude
435.912 km
Speed
7.652 km/s
True Right ascension
17h 04m 32s
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
17:39:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.29 km
Perigee altitude
434.751 km
Semi-major axis
6,818.157 km
Eccentricity
0.00077
Inclination
34.9594°
RAAN
256.1355°
Arg. of periapsis
93.1987°
True anomaly
266.87336°
Mean anomaly
266.9618°
Eccentric anomaly
266.91758°
Mean motion
3.85516 °/min
Orbital period
93.38 mins
BSTAR
0.00037366
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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 | 2025-09-17 04:28:17.484Z | 223.473° SW | 2025-09-17 04:31:17.484Z | 158.547° S | 23.343° | 2025-09-17 04:33:17.484Z | 115.694° SE |
| 4 mins | 2025-09-17 06:07:17.484Z | 235.463° WSW | 2025-09-17 06:09:17.484Z | 174.097° S | 29.397° | 2025-09-17 06:11:17.484Z | 123.701° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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