APRIZESAT 7, 39416
Orbit data source: Space-Track
APRIZESAT 7, 39416 is a payload satellite owned by SpaceQuest (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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39416 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceQuest
Mission
Operational Commercial Communications
Bus & Motor
APRIZE, Unknown motor
Mass
14 kg wet, 14 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Ant, 0.1 m
Radar Cross Section
0.060 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 APRIZESAT 7
1 39416U 13066A 25300.44267382 .00002227 00000-0 23041-3 0 9991
2 39416 97.7392 252.5962 0034718 262.7174 97.0098 14.90672617646546Epoch: 2025-10-27T10:37Z
TLE epoch observation values (Epoch: 2025-10-27T10:37:27.018Z)
Latitude
0.00006°
Longitude
57.18916°
Altitude
601.916 km
Speed
7.557 km/s
True Right ascension
16h 50m 23s
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
15:44:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
617.058 km
Perigee altitude
568.655 km
Semi-major axis
6,970.993 km
Eccentricity
0.00347
Inclination
97.7392°
RAAN
252.5962°
Arg. of periapsis
262.7174°
True anomaly
97.40445°
Mean anomaly
97.0098°
Eccentric anomaly
97.20715°
Mean motion
3.72908 °/min
Orbital period
96.54 mins
BSTAR
0.00023041
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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.APRIZESAT 7 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-27 20:25:06.137Z | 137.894° SSE | 2025-10-27 20:29:06.137Z | 57.51° ENE | 31.292° | 2025-10-27 20:32:06.137Z | 7.078° NNE |
| 4 mins | 2025-10-27 22:03:06.137Z | 244.314° WSW | 2025-10-27 22:04:06.137Z | 260.899° W | 16.319° | 2025-10-27 22:07:06.137Z | 306.854° NW |
| 6 mins | 2025-10-28 09:46:06.137Z | 17.285° NNE | 2025-10-28 09:48:06.137Z | 48.188° ENE | 43.927° | 2025-10-28 09:52:06.137Z | 189.548° 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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