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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4G 26
1 62633U 25009AA 26305.20047697 .00010194 00000-0 33249-3 0 9996
2 62633 97.3930 26.7666 0003949 156.3131 203.8294 15.31983103 99876Epoch: 2026-11-01T04:48Z
TLE epoch observation values (Epoch: 2026-11-01T04:48:41.210Z)
Latitude
0.00008°
Longitude
-85.90038°
Altitude
475.478 km
Speed
7.627 km/s
True Right ascension
01h 47m 03s
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
06:02:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.549 km
Perigee altitude
464.142 km
Semi-major axis
6,844.983 km
Eccentricity
0.00039
Inclination
97.393°
RAAN
26.7666°
Arg. of periapsis
156.3131°
True anomaly
203.81113°
Mean anomaly
203.8294°
Eccentric anomaly
203.82026°
Mean motion
3.83252 °/min
Orbital period
93.93 mins
BSTAR
0.00033249
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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 | 2026-11-01 17:54:57.699Z | 35.177° NE | 2026-11-01 17:57:57.699Z | 99.526° ESE | 30.331° | 2026-11-01 18:00:57.699Z | 160.459° S |
| 5 mins | 2026-11-02 06:01:57.699Z | 201.794° SSW | 2026-11-02 06:03:57.699Z | 266.726° W | 40.912° | 2026-11-02 06:06:57.699Z | 331.887° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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