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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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 28
1 62634U 25009AB 26238.05154360 .00008763 00000-0 25302-3 0 9991
2 62634 97.4005 322.9058 0003162 78.6414 281.5185 15.35907554 89808Epoch: 2026-08-26T01:14Z
TLE epoch observation values (Epoch: 2026-08-26T01:14:13.367Z)
Latitude
0.00002°
Longitude
-29.95999°
Altitude
460.907 km
Speed
7.636 km/s
True Right ascension
21h 31m 37s
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
02:59:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.331 km
Perigee altitude
453.01 km
Semi-major axis
6,833.308 km
Eccentricity
0.00032
Inclination
97.4005°
RAAN
322.9058°
Arg. of periapsis
78.6414°
True anomaly
281.48299°
Mean anomaly
281.5185°
Eccentric anomaly
281.50075°
Mean motion
3.84235 °/min
Orbital period
93.69 mins
BSTAR
0.00025302
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-26 18:59:23.539Z | 355.139° N | 2026-08-26 19:02:23.539Z | 279.829° WNW | 33.231° | 2026-08-26 19:05:23.539Z | 215.462° SW |
| 5 mins | 2026-08-27 05:31:23.539Z | 144.598° SSE | 2026-08-27 05:33:23.539Z | 87.681° E | 37.31° | 2026-08-27 05:36:23.539Z | 1.043° NNE |
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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