FLOCK 4G 26, 62633
Orbit data source: Space-Track
FLOCK 4G 26, 62633 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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62633 intel report (Beta)
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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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4G 26
1 62633U 25009AA 26255.67638936 .00008038 00000-0 26961-3 0 9990
2 62633 97.3973 337.3635 0003100 19.5399 340.5960 15.31153494 92295Epoch: 2026-09-12T16:14Z
TLE epoch observation values (Epoch: 2026-09-12T16:14:00.040Z)
Latitude
-0.00008°
Longitude
102.18137°
Altitude
473.472 km
Speed
7.63 km/s
True Right ascension
22h 29m 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
01:56:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.443 km
Perigee altitude
467.197 km
Semi-major axis
6,847.457 km
Eccentricity
0.00031
Inclination
97.3973°
RAAN
337.3635°
Arg. of periapsis
19.5399°
True anomaly
340.58419°
Mean anomaly
340.596°
Eccentric anomaly
340.5901°
Mean motion
3.83044 °/min
Orbital period
93.98 mins
BSTAR
0.00026961
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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 26 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 | 2026-09-13 17:53:23.070Z | 33.418° NE | 2026-09-13 17:56:23.070Z | 93.937° ESE | 31.482° | 2026-09-13 17:59:23.070Z | 159.936° S |
| 4 mins | 2026-09-14 06:01:23.070Z | 211.139° SW | 2026-09-14 06:02:23.070Z | 241.656° WSW | 37.443° | 2026-09-14 06:05:23.070Z | 326.96° NNW |
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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