CUBEBUG 2, 39440
Orbit data source: Space-Track
CUBEBUG 2, 39440 is a payload satellite owned by MinCyT (AR) 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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39440 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ARGNRelated business
Manufacturer
INVAP
Mission
Operational Amateur Technology
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, 1.0 m
Radar Cross Section
0.040 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 CUBEBUG 2
1 39440U 13066AA 25301.39094575 .00007035 00000-0 68700-3 0 9998
2 39440 97.8634 245.1645 0062485 75.4104 285.4033 14.91229764642419Epoch: 2025-10-28T09:22Z
TLE epoch observation values (Epoch: 2025-10-28T09:22:57.712Z)
Latitude
-0.00001°
Longitude
67.44492°
Altitude
585.818 km
Speed
7.573 km/s
True Right ascension
16h 20m 39s
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
17:04:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
634.671 km
Perigee altitude
547.576 km
Semi-major axis
6,969.261 km
Eccentricity
0.00625
Inclination
97.8634°
RAAN
245.1645°
Arg. of periapsis
75.4104°
True anomaly
284.71158°
Mean anomaly
285.4033°
Eccentric anomaly
285.05758°
Mean motion
3.73047 °/min
Orbital period
96.5 mins
BSTAR
0.000687
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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.CUBEBUG 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-29 08:30:35.183Z | 47.433° ENE | 2025-10-29 08:33:35.183Z | 105.962° ESE | 22.437° | 2025-10-29 08:35:35.183Z | 142.199° SSE |
| 5 mins | 2025-10-29 10:06:35.183Z | 332.042° NNW | 2025-10-29 10:08:35.183Z | 292.861° NW | 22.098° | 2025-10-29 10:11:35.183Z | 240.317° WSW |
| 6 mins | 2025-10-29 20:56:35.183Z | 204.252° SW | 2025-10-29 20:58:35.183Z | 244.668° WSW | 28.926° | 2025-10-29 21:02:35.183Z | 328.147° 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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