SKYSAT C2, 41773
Orbit data source: Space-Track
SKYSAT C2, 41773 is a payload satellite owned by Terra Bella (US) in SSO that was launched on Fri, 16 Sep 2016 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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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41773 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SS/Loral (MDA)
Mission
Operational Commercial Imaging
Bus & Motor
SKYSAT-GEN2, Unknown motor
Mass
110 kg wet, 110 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.888 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SKYSAT C2
1 41773U 16058D 25319.52981046 .00014210 00000-0 40130-3 0 9996
2 41773 97.0402 345.2228 0005548 100.7210 259.4659 15.36448764512180Epoch: 2025-11-15T12:42Z
TLE epoch observation values (Epoch: 2025-11-15T12:42:55.623Z)
Latitude
-0.00013°
Longitude
99.63342°
Altitude
460.439 km
Speed
7.636 km/s
True Right ascension
23h 00m 53s
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
15:26:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.339 km
Perigee altitude
449.759 km
Semi-major axis
6,831.686 km
Eccentricity
0.00055
Inclination
97.0402°
RAAN
345.2228°
Arg. of periapsis
100.721°
True anomaly
259.4034°
Mean anomaly
259.4659°
Eccentric anomaly
259.43465°
Mean motion
3.84372 °/min
Orbital period
93.66 mins
BSTAR
0.0004013
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Other satellites on launch #58 in the year 2016 (2016-09-16 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.SKYSAT C2 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 | 2025-11-17 02:22:42.865Z | 217.842° SW | 2025-11-17 02:23:42.865Z | 251.867° W | 30.313° | 2025-11-17 02:26:42.865Z | 328.136° NNW |
| 4 mins | 2025-11-17 15:18:42.865Z | 321.868° NNW | 2025-11-17 15:19:42.865Z | 292.282° WNW | 25.143° | 2025-11-17 15:22:42.865Z | 227.773° WSW |
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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