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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4G 24
1 62637U 25009AE 25346.94000299 .00015841 00000-0 62953-3 0 9990
2 62637 97.4197 65.3626 0002523 210.8581 149.2509 15.25388780 50493Epoch: 2025-12-12T22:33Z
TLE epoch observation values (Epoch: 2025-12-12T22:33:36.258Z)
Latitude
-0.00002°
Longitude
5.08711°
Altitude
494.205 km
Speed
7.617 km/s
True Right ascension
04h 21m 27s
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
05:23:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.309 km
Perigee altitude
484.846 km
Semi-major axis
6,864.714 km
Eccentricity
0.00025
Inclination
97.4197°
RAAN
65.3626°
Arg. of periapsis
210.8581°
True anomaly
149.26568°
Mean anomaly
149.2509°
Eccentric anomaly
149.25829°
Mean motion
3.81601 °/min
Orbital period
94.34 mins
BSTAR
0.00062953
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-13 18:00:30.538Z | 21.856° NNE | 2025-12-13 18:03:30.538Z | 71.142° E | 37.441° | 2025-12-13 18:06:30.538Z | 174.088° S |
| 4 mins | 2025-12-14 06:11:30.538Z | 228.738° WSW | 2025-12-14 06:13:30.538Z | 276.658° WNW | 20.802° | 2025-12-14 06:15:30.538Z | 313.769° NW |
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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