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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4G 7
1 62624U 25009R 26079.67592963 .00009872 00000-0 37083-3 0 9997
2 62624 97.3976 161.6131 0001219 250.8127 109.2981 15.27384580 65385Epoch: 2026-03-20T16:13Z
TLE epoch observation values (Epoch: 2026-03-20T16:13:20.320Z)
Latitude
0.00008°
Longitude
100.07084°
Altitude
487.011 km
Speed
7.622 km/s
True Right ascension
10h 46m 27s
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
19:08:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.426 km
Perigee altitude
479.754 km
Semi-major axis
6,858.727 km
Eccentricity
0.00012
Inclination
97.3976°
RAAN
161.6131°
Arg. of periapsis
250.8127°
True anomaly
109.31128°
Mean anomaly
109.2981°
Eccentric anomaly
109.30469°
Mean motion
3.82101 °/min
Orbital period
94.22 mins
BSTAR
0.00037083
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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 | 2026-03-21 17:56:26.443Z | 25.98° NE | 2026-03-21 17:59:26.443Z | 94.423° ESE | 36.004° | 2026-03-21 18:02:26.443Z | 171.782° S |
| 4 mins | 2026-03-22 04:32:26.443Z | 106.169° ESE | 2026-03-22 04:34:26.443Z | 69.044° E | 16.527° | 2026-03-22 04:36:26.443Z | 31.599° NE |
| 4 mins | 2026-03-22 06:06:26.443Z | 230.297° WSW | 2026-03-22 06:07:26.443Z | 256.392° W | 23.602° | 2026-03-22 06:10:26.443Z | 319.712° NNW |
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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