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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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4G 13
1 62621U 25009N 26171.19620215 .00066170 00000-0 13896-2 0 9995
2 62621 97.3954 254.5140 0003948 258.9336 101.1469 15.45118233 79468Epoch: 2026-06-20T04:42Z
TLE epoch observation values (Epoch: 2026-06-20T04:42:31.865Z)
Latitude
-0.00003°
Longitude
-84.53307°
Altitude
434.676 km
Speed
7.651 km/s
True Right ascension
16h 58m 03s
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
08:42:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
430.65 km
Perigee altitude
425.276 km
Semi-major axis
6,806.1 km
Eccentricity
0.00039
Inclination
97.3954°
RAAN
254.514°
Arg. of periapsis
258.9336°
True anomaly
101.19128°
Mean anomaly
101.1469°
Eccentric anomaly
101.16909°
Mean motion
3.86541 °/min
Orbital period
93.13 mins
BSTAR
0.0013896
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 05:42:19.529Z | 172.982° S | 2026-06-21 05:45:19.529Z | 316.134° NNW | 42.125° | 2026-06-21 05:47:19.529Z | 343.127° N |
| 4 mins | 2026-06-21 18:35:19.529Z | 359.647° N | 2026-06-21 18:36:19.529Z | 329.413° NNW | 41.757° | 2026-06-21 18:39:19.529Z | 200.777° SSW |
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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