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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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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 7
1 62624U 25009R 25296.48799680 .00014059 00000-0 59516-3 0 9999
2 62624 97.4166 14.8905 0004337 88.3659 271.8075 15.23280116 42799Epoch: 2025-10-23T11:42Z
TLE epoch observation values (Epoch: 2025-10-23T11:42:42.923Z)
Latitude
0.00001°
Longitude
167.06512°
Altitude
498.956 km
Speed
7.615 km/s
True Right ascension
00h 59m 33s
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
08:03:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.897 km
Perigee altitude
489.937 km
Semi-major axis
6,871.054 km
Eccentricity
0.00043
Inclination
97.4166°
RAAN
14.8905°
Arg. of periapsis
88.3659°
True anomaly
271.75783°
Mean anomaly
271.8075°
Eccentric anomaly
271.78266°
Mean motion
3.81073 °/min
Orbital period
94.47 mins
BSTAR
0.00059516
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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 | 2025-10-24 18:13:27.762Z | 11.807° NNE | 2025-10-24 18:16:27.762Z | 8.666° NNE | 44.722° | 2025-10-24 18:19:27.762Z | 193.155° SSW |
| 4 mins | 2025-10-25 04:51:27.762Z | 117.384° SE | 2025-10-25 04:53:27.762Z | 59.67° ENE | 26.887° | 2025-10-25 04:55:27.762Z | 16.742° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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