APRIZESAT 9, 40018
Orbit data source: Space-Track
APRIZESAT 9, 40018 is a payload satellite owned by SpaceQuest (US) in SSO that was launched on Thu, 19 Jun 2014 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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40018 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: 9 hours ago
TLE from 9 hours ago
0 APRIZESAT 9
1 40018U 14033J 25286.31470586 .00001234 00000-0 19062-3 0 9992
2 40018 97.8731 61.1580 0065404 274.1771 85.1965 14.73700605607199Epoch: 2025-10-13T07:33Z
TLE epoch observation values (Epoch: 2025-10-13T07:33:10.586Z)
Latitude
0.00002°
Longitude
-74.25537°
Altitude
648.742 km
Speed
7.535 km/s
True Right ascension
04h 04m 37s
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
11:09:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
692.27 km
Perigee altitude
600.384 km
Semi-major axis
7,024.464 km
Eccentricity
0.00654
Inclination
97.8731°
RAAN
61.158°
Arg. of periapsis
274.1771°
True anomaly
85.94383°
Mean anomaly
85.1965°
Eccentric anomaly
85.57012°
Mean motion
3.68658 °/min
Orbital period
97.65 mins
BSTAR
0.00019062
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Other satellites on launch #33 in the year 2014 (2014-06-19 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 9 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 | 2025-10-13 21:10:42.772Z | 42.145° NE | 2025-10-13 21:13:42.772Z | 88.596° E | 24.317° | 2025-10-13 21:17:42.772Z | 152.058° SSE |
| 6 mins | 2025-10-13 22:47:42.772Z | 341.691° N | 2025-10-13 22:50:42.772Z | 289.125° WNW | 25.767° | 2025-10-13 22:53:42.772Z | 238.674° WSW |
| 5 mins | 2025-10-14 08:09:42.772Z | 101.391° ESE | 2025-10-14 08:11:42.772Z | 66.681° ENE | 21.173° | 2025-10-14 08:14:42.772Z | 21.068° NNE |
| 6 mins | 2025-10-14 09:45:42.772Z | 211.034° SW | 2025-10-14 09:47:42.772Z | 250.035° W | 29.279° | 2025-10-14 09:51:42.772Z | 324.779° NNW |
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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