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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4G 24
1 62637U 25009AE 26095.50723933 .00014702 00000-0 53202-3 0 9993
2 62637 97.4034 178.1339 0003537 165.0336 195.1009 15.28512505 67829Epoch: 2026-04-05T12:10Z
TLE epoch observation values (Epoch: 2026-04-05T12:10:25.478Z)
Latitude
-0.00001°
Longitude
161.71607°
Altitude
485.703 km
Speed
7.621 km/s
True Right ascension
11h 52m 32s
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
23:39:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.637 km
Perigee altitude
474.788 km
Semi-major axis
6,855.35 km
Eccentricity
0.00035
Inclination
97.4034°
RAAN
178.1339°
Arg. of periapsis
165.0336°
True anomaly
195.09035°
Mean anomaly
195.1009°
Eccentric anomaly
195.09562°
Mean motion
3.82383 °/min
Orbital period
94.15 mins
BSTAR
0.00053202
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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 | 2026-04-05 19:01:20.596Z | 336.538° NNW | 2026-04-05 19:03:20.596Z | 293.417° NW | 22.601° | 2026-04-05 19:06:20.596Z | 233.719° WSW |
| 6 mins | 2026-04-06 05:35:20.596Z | 173.431° S | 2026-04-06 05:38:20.596Z | 321.226° NNW | 41.608° | 2026-04-06 05:41:20.596Z | 344.96° N |
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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