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: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4G 28
1 62634U 25009AB 26175.16221769 .00007865 00000-0 23460-3 0 9996
2 62634 97.4025 259.7376 0000204 257.9665 102.1555 15.34921133 80150Epoch: 2026-06-24T03:53Z
TLE epoch observation values (Epoch: 2026-06-24T03:53:35.608Z)
Latitude
-0.00006°
Longitude
-70.98415°
Altitude
464.295 km
Speed
7.634 km/s
True Right ascension
17h 18m 57s
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
06:50:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.24 km
Perigee altitude
457.961 km
Semi-major axis
6,836.238 km
Eccentricity
0.00002
Inclination
97.4025°
RAAN
259.7376°
Arg. of periapsis
257.9665°
True anomaly
102.15779°
Mean anomaly
102.1555°
Eccentric anomaly
102.15664°
Mean motion
3.83988 °/min
Orbital period
93.75 mins
BSTAR
0.0002346
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-25 05:04:10.948Z | 123.804° SE | 2026-06-25 05:06:10.948Z | 84.292° E | 22.596° | 2026-06-25 05:09:10.948Z | 17.282° NNE |
| 4 mins | 2026-06-25 18:02:10.948Z | 62.179° ENE | 2026-06-25 18:03:10.948Z | 93.729° ESE | 26.786° | 2026-06-25 18:06:10.948Z | 159.733° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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