GOMX 1, 39430
Orbit data source: Space-Track
GOMX 1, 39430 is a payload satellite owned by GOMSpace (DK) 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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39430 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
DK / DENRelated business
Manufacturer
GOMSP/AAU
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.075 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 GOMX 1
1 39430U 13066Q 25300.56611438 .00002626 00000-0 40596-3 0 9992
2 39430 97.6646 150.5790 0132394 103.9081 257.6892 14.68286269635768Epoch: 2025-10-27T13:35Z
TLE epoch observation values (Epoch: 2025-10-27T13:35:12.282Z)
Latitude
-0.00002°
Longitude
-89.38829°
Altitude
690.622 km
Speed
7.5 km/s
True Right ascension
10h 02m 18s
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
15:39:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
756.818 km
Perigee altitude
570.361 km
Semi-major axis
7,041.727 km
Eccentricity
0.01324
Inclination
97.6646°
RAAN
150.579°
Arg. of periapsis
103.9081°
True anomaly
256.21234°
Mean anomaly
257.6892°
Eccentric anomaly
256.95023°
Mean motion
3.67303 °/min
Orbital period
98.01 mins
BSTAR
0.00040596
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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.GOMX 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-28 03:14:28.574Z | 1.973° NNE | 2025-10-28 03:17:28.574Z | 285.492° WNW | 41.403° | 2025-10-28 03:21:28.574Z | 205.078° SW |
| 6 mins | 2025-10-28 14:15:28.574Z | 174.224° S | 2025-10-28 14:18:28.574Z | 312.964° NW | 43.003° | 2025-10-28 14:21:28.574Z | 343.754° N |
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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