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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4G 7
1 62624U 25009R 26126.50067458 .00009160 00000-0 33318-3 0 9995
2 62624 97.3942 208.0833 0004318 107.8618 252.3093 15.28460245 72535Epoch: 2026-05-06T12:00Z
TLE epoch observation values (Epoch: 2026-05-06T12:00:58.283Z)
Latitude
-0.00004°
Longitude
163.48019°
Altitude
484.418 km
Speed
7.623 km/s
True Right ascension
13h 52m 19s
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
03:08:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.329 km
Perigee altitude
474.408 km
Semi-major axis
6,855.506 km
Eccentricity
0.00043
Inclination
97.3942°
RAAN
208.0833°
Arg. of periapsis
107.8618°
True anomaly
252.26217°
Mean anomaly
252.3093°
Eccentric anomaly
252.28573°
Mean motion
3.8237 °/min
Orbital period
94.15 mins
BSTAR
0.00033318
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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 | 2026-05-07 05:25:45.555Z | 164.803° S | 2026-05-07 05:28:45.555Z | 9.384° NNE | 44.129° | 2026-05-07 05:31:45.555Z | 349.486° N |
| 5 mins | 2026-05-07 18:26:45.555Z | 0.956° NNE | 2026-05-07 18:28:45.555Z | 259.823° W | 42.555° | 2026-05-07 18:31:45.555Z | 201.418° 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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