CYGFM08, 41888
Orbit data source: Space-Track
CYGFM08, 41888 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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41888 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: 5 hours ago
TLE from 5 hours ago
0 CYGFM08
1 41888U 16078E 26034.12618385 .00024553 00000-0 39207-3 0 9993
2 41888 34.9453 48.6166 0008757 321.0194 38.9897 15.52161321508078Epoch: 2026-02-03T03:01Z
TLE epoch observation values (Epoch: 2026-02-03T03:01:42.284Z)
Latitude
-0.00002°
Longitude
-130.12121°
Altitude
404.687 km
Speed
7.673 km/s
True Right ascension
03h 14m 27s
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
09:52:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419.665 km
Perigee altitude
407.769 km
Semi-major axis
6,791.854 km
Eccentricity
0.00088
Inclination
34.9453°
RAAN
48.6166°
Arg. of periapsis
321.0194°
True anomaly
39.05289°
Mean anomaly
38.9897°
Eccentric anomaly
39.02129°
Mean motion
3.87758 °/min
Orbital period
92.84 mins
BSTAR
0.00039207
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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.CYGFM08 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 | 2026-02-03 08:03:02.329Z | 242.1° WSW | 2026-02-03 08:05:02.329Z | 191.428° SSW | 26.755° | 2026-02-03 08:08:02.329Z | 124.816° SE |
| 4 mins | 2026-02-04 05:34:02.329Z | 214.628° SW | 2026-02-04 05:36:02.329Z | 158.891° S | 24.045° | 2026-02-04 05:38:02.329Z | 115.109° SE |
| 4 mins | 2026-02-04 07:12:02.329Z | 225.288° WSW | 2026-02-04 07:13:02.329Z | 192.642° SSW | 28.089° | 2026-02-04 07:16:02.329Z | 120.448° 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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