SKYSAT C1, 41601
Orbit data source: Space-Track
SKYSAT C1, 41601 is a payload satellite owned by Terra Bella (US) in SSO that was launched on Wed, 22 Jun 2016 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). 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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41601 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 C1
1 41601U 16040C 25301.58711067 .00011597 00000-0 38434-3 0 9997
2 41601 96.9893 341.1662 0004299 116.9756 243.1926 15.31413294522368Epoch: 2025-10-28T14:05Z
TLE epoch observation values (Epoch: 2025-10-28T14:05:26.361Z)
Latitude
-0.00004°
Longitude
92.6339°
Altitude
476.042 km
Speed
7.627 km/s
True Right ascension
22h 44m 39s
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
09:41:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.471 km
Perigee altitude
465.585 km
Semi-major axis
6,846.665 km
Eccentricity
0.00043
Inclination
96.9893°
RAAN
341.1662°
Arg. of periapsis
116.9756°
True anomaly
243.14864°
Mean anomaly
243.1926°
Eccentric anomaly
243.17062°
Mean motion
3.83111 °/min
Orbital period
93.97 mins
BSTAR
0.00038434
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Other satellites on launch #40 in the year 2016 (2016-06-22 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 C1 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-29 15:44:39.183Z | 4.801° NNE | 2025-10-29 15:47:39.183Z | 238.462° WSW | 41.642° | 2025-10-29 15:50:39.183Z | 199.766° SSW |
| 4 mins | 2025-10-30 02:18:39.183Z | 121.5° SE | 2025-10-30 02:20:39.183Z | 64.876° ENE | 26.997° | 2025-10-30 02:22:39.183Z | 18.139° NNE |
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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