FLOCK 4G 28, 62634
Orbit data source: Space-Track
FLOCK 4G 28, 62634 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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62634 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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 28
1 62634U 25009AB 25322.13512670 .00009892 00000-0 33798-3 0 9997
2 62634 97.4213 41.3600 0001856 18.0522 342.0784 15.30495101 46750Epoch: 2025-11-18T03:14Z
TLE epoch observation values (Epoch: 2025-11-18T03:14:34.946Z)
Latitude
-0.00008°
Longitude
-64.71116°
Altitude
476.228 km
Speed
7.628 km/s
True Right ascension
02h 45m 26s
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
09:21:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.558 km
Perigee altitude
470.015 km
Semi-major axis
6,849.424 km
Eccentricity
0.00019
Inclination
97.4213°
RAAN
41.36°
Arg. of periapsis
18.0522°
True anomaly
342.07185°
Mean anomaly
342.0784°
Eccentric anomaly
342.07513°
Mean motion
3.8288 °/min
Orbital period
94.02 mins
BSTAR
0.00033798
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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 28 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 | 2025-11-19 17:29:20.095Z | 60.869° ENE | 2025-11-19 17:31:20.095Z | 102.863° ESE | 17.288° | 2025-11-19 17:33:20.095Z | 138.635° SSE |
| 5 mins | 2025-11-20 05:35:20.095Z | 175.556° S | 2025-11-20 05:37:20.095Z | 207.799° SW | 42.007° | 2025-11-20 05:40:20.095Z | 342.237° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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