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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Identifier
Orbit
Country
AR / 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: 9 hours ago
TLE from 9 hours ago
0 CUBEBUG 2
1 39440U 13066AA 26092.28730929 .00006323 00000-0 59187-3 0 9992
2 39440 97.8852 41.0067 0056465 279.5440 79.9401 14.93229168665660Epoch: 2026-04-02T06:53Z
TLE epoch observation values (Epoch: 2026-04-02T06:53:43.522Z)
Latitude
-0.00006°
Longitude
106.93741°
Altitude
584.258 km
Speed
7.572 km/s
True Right ascension
02h 44m 01s
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
21:55:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.214 km
Perigee altitude
545.58 km
Semi-major axis
6,963.034 km
Eccentricity
0.00565
Inclination
97.8852°
RAAN
41.0067°
Arg. of periapsis
279.544°
True anomaly
80.57797°
Mean anomaly
79.9401°
Eccentric anomaly
80.25896°
Mean motion
3.73547 °/min
Orbital period
96.37 mins
BSTAR
0.00059187
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-02 19:53:45.631Z | 130.565° SE | 2026-04-02 19:56:45.631Z | 79.302° E | 28.035° | 2026-04-02 20:00:45.631Z | 7.929° NNE |
| 4 mins | 2026-04-02 21:30:45.631Z | 233.935° WSW | 2026-04-02 21:32:45.631Z | 270.131° WNW | 18.901° | 2026-04-02 21:34:45.631Z | 303.618° NW |
| 6 mins | 2026-04-03 09:12:45.631Z | 24.373° NE | 2026-04-03 09:15:45.631Z | 125.359° SE | 41.27° | 2026-04-03 09:18:45.631Z | 180.381° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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