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 26261.44587588 .00006816 00000-0 23080-3 0 9999
2 62624 97.3882 342.3117 0002358 24.5274 335.6079 15.30906032 93163Epoch: 2026-09-18T10:42Z
TLE epoch observation values (Epoch: 2026-09-18T10:42:03.676Z)
Latitude
0.00002°
Longitude
-175.57227°
Altitude
474.742 km
Speed
7.629 km/s
True Right ascension
22h 49m 14s
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
06:37:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.673 km
Perigee altitude
468.444 km
Semi-major axis
6,848.195 km
Eccentricity
0.00024
Inclination
97.3882°
RAAN
342.3117°
Arg. of periapsis
24.5274°
True anomaly
335.59674°
Mean anomaly
335.6079°
Eccentric anomaly
335.60232°
Mean motion
3.82983 °/min
Orbital period
94 mins
BSTAR
0.0002308
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-19 18:37:57.307Z | 359.624° N | 2026-09-19 18:40:57.307Z | 274.859° WNW | 52.47° | 2026-09-19 18:43:57.307Z | 208.978° SW |
| 5 mins | 2026-09-20 05:11:57.307Z | 138.005° SSE | 2026-09-20 05:13:57.307Z | 81.824° E | 43.341° | 2026-09-20 05:16:57.307Z | 4.425° NNE |
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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