FLOCK 4G 7, 62624
Orbit data source: Space-Track
FLOCK 4G 7, 62624 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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62624 intel report (Beta)
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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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 7
1 62624U 25009R 26215.81196668 .00009438 00000-0 32523-3 0 9999
2 62624 97.3922 296.8838 0003974 133.5049 226.6523 15.30224112 86186Epoch: 2026-08-03T19:29Z
TLE epoch observation values (Epoch: 2026-08-03T19:29:13.921Z)
Latitude
0.00004°
Longitude
52.18608°
Altitude
480.118 km
Speed
7.624 km/s
True Right ascension
19h 47m 32s
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
19:59:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
474.817 km
Perigee altitude
469.372 km
Semi-major axis
6,850.232 km
Eccentricity
0.0004
Inclination
97.3922°
RAAN
296.8838°
Arg. of periapsis
133.5049°
True anomaly
226.6192°
Mean anomaly
226.6523°
Eccentric anomaly
226.63575°
Mean motion
3.82812 °/min
Orbital period
94.04 mins
BSTAR
0.00032523
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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 7 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 | 2026-08-05 06:09:00.073Z | 215.176° SW | 2026-08-05 06:11:00.073Z | 262.234° W | 24.002° | 2026-08-05 06:14:00.073Z | 322.252° NNW |
| 5 mins | 2026-08-06 05:42:00.073Z | 185.104° SSW | 2026-08-06 05:44:00.073Z | 291.972° WNW | 40.936° | 2026-08-06 05:47:00.073Z | 341.395° 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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