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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Edit Public Description
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: 22 hours ago
TLE from 22 hours ago
0 DOVE 3
1 39429U 13066P 25300.61808946 .00003921 00000-0 53449-3 0 9998
2 39429 97.6881 167.1880 0118908 58.7172 302.5618 14.74387171636717Epoch: 2025-10-27T14:50Z
TLE epoch observation values (Epoch: 2025-10-27T14:50:02.929Z)
Latitude
-0.00001°
Longitude
-91.54155°
Altitude
605.861 km
Speed
7.58 km/s
True Right ascension
11h 08m 45s
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
07:53:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
727.636 km
Perigee altitude
560.635 km
Semi-major axis
7,022.273 km
Eccentricity
0.01189
Inclination
97.6881°
RAAN
167.188°
Arg. of periapsis
58.7172°
True anomaly
301.40422°
Mean anomaly
302.5618°
Eccentric anomaly
301.98393°
Mean motion
3.6883 °/min
Orbital period
97.61 mins
BSTAR
0.00053449
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Other satellites on launch #66 in the year 2013 (2013-11-21 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-28 15:23:12.812Z | 174.795° S | 2025-10-28 15:26:12.812Z | 217.639° SW | 42.439° | 2025-10-28 15:30:12.812Z | 342.768° N |
| 6 mins | 2025-10-29 03:15:12.812Z | 51.791° ENE | 2025-10-29 03:17:12.812Z | 85.344° E | 21.591° | 2025-10-29 03:21:12.812Z | 148.636° SSE |
| 5 mins | 2025-10-29 04:52:12.812Z | 333.657° NNW | 2025-10-29 04:54:12.812Z | 292.512° NW | 26.025° | 2025-10-29 04:57:12.812Z | 237.315° WSW |
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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