CYGFM02, 41886
Orbit data source: Space-Track
CYGFM02, 41886 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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41886 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: 11 hours ago
TLE from 11 hours ago
0 CYGFM02
1 41886U 16078C 26135.26296734 .00019935 00000-0 21971-3 0 9995
2 41886 34.9406 83.0397 0009508 249.8420 110.1284 15.62066725524015Epoch: 2026-05-15T06:18Z
TLE epoch observation values (Epoch: 2026-05-15T06:18:40.378Z)
Latitude
0.00005°
Longitude
115.37472°
Altitude
382.787 km
Speed
7.681 km/s
True Right ascension
05h 32m 09s
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
01:31:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
391.433 km
Perigee altitude
378.573 km
Semi-major axis
6,763.14 km
Eccentricity
0.00095
Inclination
34.9406°
RAAN
83.0397°
Arg. of periapsis
249.842°
True anomaly
110.23066°
Mean anomaly
110.1284°
Eccentric anomaly
110.17953°
Mean motion
3.9023 °/min
Orbital period
92.25 mins
BSTAR
0.00021971
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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.CYGFM02 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 | 2026-05-16 00:59:36.585Z | 208.752° SW | 2026-05-16 01:01:36.585Z | 158.995° S | 20.273° | 2026-05-16 01:03:36.585Z | 116.332° SE |
| 4 mins | 2026-05-16 02:36:36.585Z | 231.093° WSW | 2026-05-16 02:38:36.585Z | 164.251° S | 27.055° | 2026-05-16 02:40:36.585Z | 119.642° 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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