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: 12 hours ago
TLE from 12 hours ago
0 FLOCK 4G 24
1 62637U 25009AE 26095.17991232 .00014524 00000-0 52577-3 0 9991
2 62637 97.4034 177.8083 0003463 165.6833 194.4505 15.28502882 67771Epoch: 2026-04-05T04:19Z
TLE epoch observation values (Epoch: 2026-04-05T04:19:04.424Z)
Latitude
-0.00007°
Longitude
-80.44917°
Altitude
485.689 km
Speed
7.621 km/s
True Right ascension
11h 51m 13s
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
21:55:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.615 km
Perigee altitude
474.867 km
Semi-major axis
6,855.378 km
Eccentricity
0.00035
Inclination
97.4034°
RAAN
177.8083°
Arg. of periapsis
165.6833°
True anomaly
194.4406°
Mean anomaly
194.4505°
Eccentric anomaly
194.44555°
Mean motion
3.82381 °/min
Orbital period
94.15 mins
BSTAR
0.00052577
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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 | 2026-04-05 17:28:07.647Z | 55.675° ENE | 2026-04-05 17:30:07.647Z | 93.389° ESE | 16.657° | 2026-04-05 17:32:07.647Z | 131.698° SE |
| 4 mins | 2026-04-05 19:02:07.647Z | 323.779° NNW | 2026-04-05 19:03:07.647Z | 299.583° NW | 22.3° | 2026-04-05 19:06:07.647Z | 235.867° WSW |
| 5 mins | 2026-04-06 05:36:07.647Z | 176.034° S | 2026-04-06 05:38:07.647Z | 305.178° NW | 43.401° | 2026-04-06 05:41:07.647Z | 344.648° 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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