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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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: 20 hours ago
TLE from 20 hours ago
0 CYGFM08
1 41888U 16078E 26278.11801500 .00041486 00000-0 39010-3 0 9991
2 41888 34.9412 226.2874 0005968 181.7720 178.2986 15.66002973546183Epoch: 2026-10-05T02:49Z
TLE epoch observation values (Epoch: 2026-10-05T02:49:56.496Z)
Latitude
-0.00003°
Longitude
170.00045°
Altitude
373.261 km
Speed
7.686 km/s
True Right ascension
15h 05m 08s
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
16:44:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
377.706 km
Perigee altitude
369.647 km
Semi-major axis
6,751.813 km
Eccentricity
0.0006
Inclination
34.9412°
RAAN
226.2874°
Arg. of periapsis
181.772°
True anomaly
178.30063°
Mean anomaly
178.2986°
Eccentric anomaly
178.29961°
Mean motion
3.91212 °/min
Orbital period
92.02 mins
BSTAR
0.0003901
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-06 02:06:30.484Z | 226.632° WSW | 2026-10-06 02:08:30.484Z | 163.269° S | 29.504° | 2026-10-06 02:10:30.484Z | 115.962° 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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