DOVE 3, 39429
Orbit data source: Space-Track
DOVE 3, 39429 is a payload satellite owned by Planet Labs (US) 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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39429 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet Labs
Mission
Non-operational Commercial Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5.2 kg wet, 5.2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.092 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 DOVE 3
1 39429U 13066P 26092.03141639 .00003326 00000-0 44412-3 0 9991
2 39429 97.6727 315.7540 0113059 271.9421 86.8845 14.75834979659777Epoch: 2026-04-02T00:45Z
TLE epoch observation values (Epoch: 2026-04-02T00:45:14.376Z)
Latitude
0.00004°
Longitude
114.05836°
Altitude
642.106 km
Speed
7.539 km/s
True Right ascension
21h 03m 00s
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
19:58:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
718.879 km
Perigee altitude
560.197 km
Semi-major axis
7,017.675 km
Eccentricity
0.01131
Inclination
97.6727°
RAAN
315.754°
Arg. of periapsis
271.9421°
True anomaly
88.17903°
Mean anomaly
86.8845°
Eccentric anomaly
87.53168°
Mean motion
3.69193 °/min
Orbital period
97.51 mins
BSTAR
0.00044412
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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.DOVE 3 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-02 15:30:28.477Z | 198.036° SSW | 2026-04-02 15:34:28.477Z | 260.596° W | 29.873° | 2026-04-02 15:38:28.477Z | 327.071° NNW |
| 8 mins | 2026-04-03 03:22:28.477Z | 26.173° NE | 2026-04-03 03:26:28.477Z | 121.388° SE | 37.805° | 2026-04-03 03:30:28.477Z | 176.481° S |
| 4 mins | 2026-04-03 05:00:28.477Z | 319.676° NNW | 2026-04-03 05:02:28.477Z | 290.308° WNW | 15.685° | 2026-04-03 05:04:28.477Z | 263.083° W |
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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