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, 0.6 m
Radar Cross Section
0.888 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 SKYSAT C2
1 41773U 16058D 25261.07403968 .00009149 00000-0 27523-3 0 9990
2 41773 97.0487 289.3327 0002381 349.4422 10.6771 15.34582608503210Epoch: 2025-09-18T01:46Z
TLE epoch observation values (Epoch: 2025-09-18T01:46:37.028Z)
Latitude
-0.00008°
Longitude
-94.56244°
Altitude
463.68 km
Speed
7.636 km/s
True Right ascension
19h 17m 19s
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
09:53:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.72 km
Perigee altitude
457.464 km
Semi-major axis
6,837.229 km
Eccentricity
0.00024
Inclination
97.0487°
RAAN
289.3327°
Arg. of periapsis
349.4422°
True anomaly
10.68216°
Mean anomaly
10.6771°
Eccentric anomaly
10.67963°
Mean motion
3.83904 °/min
Orbital period
93.77 mins
BSTAR
0.00027523
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-19 01:23:16.702Z | 127.594° SE | 2025-09-19 01:26:16.702Z | 64.937° ENE | 22.816° | 2025-09-19 01:28:16.702Z | 21.965° NNE |
| 4 mins | 2025-09-19 14:21:16.702Z | 48.782° ENE | 2025-09-19 14:23:16.702Z | 111.829° ESE | 27.848° | 2025-09-19 14:25:16.702Z | 156.453° SSE |
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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