SKYSAT 2, 40072
Orbit data source: Space-Track
SKYSAT 2, 40072 is a payload satellite owned by Skybox (US) in SSO that was launched on Tue, 08 Jul 2014 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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40072 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Skybox
Mission
Operational Commercial Imaging
Bus & Motor
SKYSAT, Unknown motor
Mass
82 kg wet, 82 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.800 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 SKYSAT 2
1 40072U 14037D 25260.89606921 .00001589 00000-0 18500-3 0 9994
2 40072 98.3462 200.1769 0007321 82.5288 277.6758 14.86801840605483Epoch: 2025-09-17T21:30Z
TLE epoch observation values (Epoch: 2025-09-17T21:30:20.379Z)
Latitude
-0.00003°
Longitude
-119.47345°
Altitude
610.273 km
Speed
7.554 km/s
True Right ascension
13h 20m 42s
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
07:21:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
610.101 km
Perigee altitude
599.876 km
Semi-major axis
6,983.125 km
Eccentricity
0.00073
Inclination
98.3462°
RAAN
200.1769°
Arg. of periapsis
82.5288°
True anomaly
277.59265°
Mean anomaly
277.6758°
Eccentric anomaly
277.63423°
Mean motion
3.71936 °/min
Orbital period
96.79 mins
BSTAR
0.000185
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Other satellites on launch #37 in the year 2014 (2014-07-08 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SKYSAT 2 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 | 2025-09-18 20:15:01.328Z | 180.774° SSW | 2025-09-18 20:18:01.328Z | 278.363° WNW | 41.539° | 2025-09-18 20:21:01.328Z | 337.722° N |
| 4 mins | 2025-09-19 08:02:01.328Z | 68.635° E | 2025-09-19 08:03:01.328Z | 86.469° E | 18.313° | 2025-09-19 08:06:01.328Z | 136.547° SSE |
| 6 mins | 2025-09-19 09:37:01.328Z | 340.537° N | 2025-09-19 09:39:01.328Z | 298.527° NW | 28.243° | 2025-09-19 09:43:01.328Z | 226.61° WSW |
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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