FLOCK 4G 24, 62637
Orbit data source: Space-Track
FLOCK 4G 24, 62637 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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62637 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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 24
1 62637U 25009AE 26215.81055315 .00009459 00000-0 32091-3 0 9999
2 62637 97.4004 297.9341 0004636 116.8593 243.3123 15.30726785 86216Epoch: 2026-08-03T19:27Z
TLE epoch observation values (Epoch: 2026-08-03T19:27:11.792Z)
Latitude
0.00006°
Longitude
53.74664°
Altitude
478.176 km
Speed
7.626 km/s
True Right ascension
19h 51m 44s
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
19:51:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.769 km
Perigee altitude
467.419 km
Semi-major axis
6,848.731 km
Eccentricity
0.00046
Inclination
97.4004°
RAAN
297.9341°
Arg. of periapsis
116.8593°
True anomaly
243.26485°
Mean anomaly
243.3123°
Eccentric anomaly
243.28857°
Mean motion
3.82938 °/min
Orbital period
94.01 mins
BSTAR
0.00032091
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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 24 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 06:05:36.207Z | 200.328° SSW | 2026-08-05 06:08:36.207Z | 271.495° WNW | 27.855° | 2026-08-05 06:10:36.207Z | 318.974° NNW |
| 4 mins | 2026-08-05 19:05:36.207Z | 327.191° NNW | 2026-08-05 19:07:36.207Z | 274.344° WNW | 22.4° | 2026-08-05 19:09:36.207Z | 236.218° WSW |
| 5 mins | 2026-08-06 05:38:36.207Z | 171.484° S | 2026-08-06 05:40:36.207Z | 271.372° WNW | 44.75° | 2026-08-06 05:43:36.207Z | 346.02° N |
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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