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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Edit Public Description
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: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4G 24
1 62637U 25009AE 25300.47288926 .00011793 00000-0 49108-3 0 9992
2 62637 97.4234 19.3279 0004057 53.1357 307.0252 15.23883608 43411Epoch: 2025-10-27T11:20Z
TLE epoch observation values (Epoch: 2025-10-27T11:20:57.632Z)
Latitude
0.00004°
Longitude
173.01353°
Altitude
495.556 km
Speed
7.618 km/s
True Right ascension
01h 17m 18s
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
01:23:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.888 km
Perigee altitude
488.314 km
Semi-major axis
6,869.238 km
Eccentricity
0.00041
Inclination
97.4234°
RAAN
19.3279°
Arg. of periapsis
53.1357°
True anomaly
306.98807°
Mean anomaly
307.0252°
Eccentric anomaly
307.00664°
Mean motion
3.81224 °/min
Orbital period
94.43 mins
BSTAR
0.00049108
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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 | 2025-10-28 06:23:51.451Z | 232.123° WSW | 2025-10-28 06:25:51.451Z | 268.228° W | 15.179° | 2025-10-28 06:27:51.451Z | 303.231° NW |
| 4 mins | 2025-10-28 17:52:51.451Z | 46.819° ENE | 2025-10-28 17:54:51.451Z | 121.249° SE | 31.79° | 2025-10-28 17:56:51.451Z | 163.681° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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