FLOCK 4G 3, 62639
Orbit data source: Space-Track
FLOCK 4G 3, 62639 is a payload satellite owned by Planet (US) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62639 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5.7 kg wet, 5.7 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.072 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 FLOCK 4G 3
1 62639U 25009AG 25346.20192689 .00015500 00000-0 62280-3 0 9991
2 62639 97.4197 64.5104 0002102 219.7562 140.3522 15.25026639 50362Epoch: 2025-12-12T04:50Z
TLE epoch observation values (Epoch: 2025-12-12T04:50:46.483Z)
Latitude
-0.00001°
Longitude
-89.33022°
Altitude
494.914 km
Speed
7.617 km/s
True Right ascension
04h 18m 02s
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
16:00:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.108 km
Perigee altitude
486.222 km
Semi-major axis
6,865.802 km
Eccentricity
0.00021
Inclination
97.4197°
RAAN
64.5104°
Arg. of periapsis
219.7562°
True anomaly
140.36757°
Mean anomaly
140.3522°
Eccentric anomaly
140.35988°
Mean motion
3.8151 °/min
Orbital period
94.36 mins
BSTAR
0.0006228
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.FLOCK 4G 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-12 18:00:16.735Z | 22.905° NE | 2025-12-12 18:03:16.735Z | 87.988° E | 38.713° | 2025-12-12 18:06:16.735Z | 175.587° S |
| 4 mins | 2025-12-13 06:11:16.735Z | 230.391° WSW | 2025-12-13 06:12:16.735Z | 252.645° W | 20.778° | 2025-12-13 06:15:16.735Z | 314.625° NW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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