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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4G 24
1 62637U 25009AE 26307.48044679 .00006839 00000-0 22179-3 0 9990
2 62637 97.3942 29.3993 0004022 138.2804 221.8745 15.32299040100240Epoch: 2026-11-03T11:31Z
TLE epoch observation values (Epoch: 2026-11-03T11:31:50.602Z)
Latitude
-0.00005°
Longitude
173.69596°
Altitude
474.114 km
Speed
7.628 km/s
True Right ascension
01h 57m 35s
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
17:12:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.656 km
Perigee altitude
463.151 km
Semi-major axis
6,844.041 km
Eccentricity
0.0004
Inclination
97.3942°
RAAN
29.3993°
Arg. of periapsis
138.2804°
True anomaly
221.84375°
Mean anomaly
221.8745°
Eccentric anomaly
221.85912°
Mean motion
3.83331 °/min
Orbital period
93.91 mins
BSTAR
0.00022179
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-04 04:55:11.735Z | 115.16° SE | 2026-11-04 04:57:11.735Z | 74.431° E | 21.765° | 2026-11-04 04:59:11.735Z | 29.901° NE |
| 4 mins | 2026-11-04 17:54:11.735Z | 64.768° ENE | 2026-11-04 17:55:11.735Z | 92.916° ESE | 26.72° | 2026-11-04 17:58:11.735Z | 155.28° SSE |
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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