SKYSAT 1, 39418
Orbit data source: Space-Track
SKYSAT 1, 39418 is a payload satellite owned by Skybox (US) in SSO that was launched on Thu, 21 Nov 2013 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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39418 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Skybox
Mission
Operational Commercial Imaging
Bus & Motor
SKYSTAT, Unknown motor
Mass
90 kg wet, 90 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.800 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 SKYSAT 1
1 39418U 13066C 25300.39531109 .00004007 00000-0 24153-3 0 9991
2 39418 97.4174 352.0101 0023362 42.1411 318.1610 15.11102952653304Epoch: 2025-10-27T09:29Z
TLE epoch observation values (Epoch: 2025-10-27T09:29:14.878Z)
Latitude
-0.00002°
Longitude
173.70034°
Altitude
523.899 km
Speed
7.608 km/s
True Right ascension
23h 28m 02s
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
18:25:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.952 km
Perigee altitude
513.675 km
Semi-major axis
6,907.95 km
Eccentricity
0.00234
Inclination
97.4174°
RAAN
352.0101°
Arg. of periapsis
42.1411°
True anomaly
317.98204°
Mean anomaly
318.161°
Eccentric anomaly
318.07156°
Mean motion
3.78024 °/min
Orbital period
95.23 mins
BSTAR
0.00024153
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Other satellites on launch #66 in the year 2013 (2013-11-21 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 1 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 | 2025-10-28 03:05:44.436Z | 138.975° SSE | 2025-10-28 03:08:44.436Z | 87.894° E | 29.29° | 2025-10-28 03:11:44.436Z | 12.501° NNE |
| 6 mins | 2025-10-28 16:15:44.436Z | 24.705° NE | 2025-10-28 16:17:44.436Z | 80.243° E | 41.512° | 2025-10-28 16:21:44.436Z | 182.875° SSW |
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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