FLOCK 4G 21, 62651
Orbit data source: Space-Track
FLOCK 4G 21, 62651 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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62651 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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4G 21
1 62651U 25009AU 25335.22821437 .00013741 00000-0 54335-3 0 9992
2 62651 97.4185 53.8451 0000541 292.4307 67.6874 15.25591547 48722Epoch: 2025-12-01T05:28Z
TLE epoch observation values (Epoch: 2025-12-01T05:28:37.721Z)
Latitude
-0.00001°
Longitude
-98.6428°
Altitude
491.966 km
Speed
7.619 km/s
True Right ascension
03h 35m 22s
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
11:44:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.34 km
Perigee altitude
485.597 km
Semi-major axis
6,864.106 km
Eccentricity
0.00005
Inclination
97.4185°
RAAN
53.8451°
Arg. of periapsis
292.4307°
True anomaly
67.69314°
Mean anomaly
67.6874°
Eccentric anomaly
67.69027°
Mean motion
3.81652 °/min
Orbital period
94.33 mins
BSTAR
0.00054335
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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 21 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 | 2025-12-01 18:37:16.715Z | 358.294° N | 2025-12-01 18:40:16.715Z | 302.33° NW | 34.608° | 2025-12-01 18:43:16.715Z | 216.934° SW |
| 5 mins | 2025-12-02 05:14:16.715Z | 144.954° SSE | 2025-12-02 05:16:16.715Z | 58.301° ENE | 39.819° | 2025-12-02 05:19:16.715Z | 357.392° N |
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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