DTUSAT 2, 40030
Orbit data source: Space-Track
DTUSAT 2, 40030 is a payload satellite owned by DTU (DK) 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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40030 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
DK / DENRelated business
Manufacturer
DTU
Mission
Operational Amateur Communications
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1.333 kg wet, 1.333 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 DTUSAT 2
1 40030U 14033W 25287.93133771 .00009812 00000-0 60212-3 0 9990
2 40030 98.0707 266.1687 0008725 6.1522 353.9811 15.10313346615609Epoch: 2025-10-14T22:21Z
TLE epoch observation values (Epoch: 2025-10-14T22:21:07.578Z)
Latitude
-0.00005°
Longitude
-92.82555°
Altitude
532.301 km
Speed
7.6 km/s
True Right ascension
17h 44m 40s
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
09:02:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.281 km
Perigee altitude
526.223 km
Semi-major axis
6,910.389 km
Eccentricity
0.00087
Inclination
98.0707°
RAAN
266.1687°
Arg. of periapsis
6.1522°
True anomaly
353.9706°
Mean anomaly
353.9811°
Eccentric anomaly
353.97585°
Mean motion
3.77824 °/min
Orbital period
95.28 mins
BSTAR
0.00060212
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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.DTUSAT 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-15 22:19:41.076Z | 146.908° SSE | 2025-10-15 22:22:41.076Z | 95.784° ESE | 35.722° | 2025-10-15 22:26:41.076Z | 359.208° N |
| 7 mins | 2025-10-16 11:28:41.076Z | 15.981° NNE | 2025-10-16 11:32:41.076Z | 148.792° SSE | 43.457° | 2025-10-16 11:35:41.076Z | 188.306° 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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