FLOCK 4G 13, 62621
Orbit data source: Space-Track
FLOCK 4G 13, 62621 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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62621 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 13
1 62621U 25009N 25326.52630602 .00011452 00000-0 47642-3 0 9994
2 62621 97.4198 44.5906 0005343 346.9175 13.1923 15.23919040 47346Epoch: 2025-11-22T12:37Z
TLE epoch observation values (Epoch: 2025-11-22T12:37:52.840Z)
Latitude
0.00002°
Longitude
153.36671°
Altitude
493.553 km
Speed
7.62 km/s
True Right ascension
02h 58m 21s
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
18:48:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.665 km
Perigee altitude
487.324 km
Semi-major axis
6,869.131 km
Eccentricity
0.00053
Inclination
97.4198°
RAAN
44.5906°
Arg. of periapsis
346.9175°
True anomaly
13.20628°
Mean anomaly
13.1923°
Eccentric anomaly
13.19929°
Mean motion
3.81233 °/min
Orbital period
94.43 mins
BSTAR
0.00047642
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.FLOCK 4G 13 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-23 04:32:34.650Z | 109.489° ESE | 2025-11-23 04:34:34.650Z | 72.195° E | 17.84° | 2025-11-23 04:36:34.650Z | 32.456° NE |
| 4 mins | 2025-11-23 06:06:34.650Z | 225.668° WSW | 2025-11-23 06:08:34.650Z | 275.047° WNW | 22.088° | 2025-11-23 06:10:34.650Z | 314.068° NW |
| 4 mins | 2025-11-23 17:35:34.650Z | 64.099° ENE | 2025-11-23 17:36:34.650Z | 89.396° E | 23.24° | 2025-11-23 17:39:34.650Z | 151.196° SSE |
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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