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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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: 11 hours ago
TLE from 11 hours ago
0 FLOCK 4G 26
1 62633U 25009AA 25326.45957315 .00012024 00000-0 49082-3 0 9998
2 62633 97.4216 44.9213 0002605 328.4362 31.6719 15.24554257 47362Epoch: 2025-11-22T11:01Z
TLE epoch observation values (Epoch: 2025-11-22T11:01:47.120Z)
Latitude
0°
Longitude
177.78703°
Altitude
493.697 km
Speed
7.619 km/s
True Right ascension
02h 59m 41s
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
18:46:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.874 km
Perigee altitude
487.296 km
Semi-major axis
6,867.222 km
Eccentricity
0.00026
Inclination
97.4216°
RAAN
44.9213°
Arg. of periapsis
328.4362°
True anomaly
31.68758°
Mean anomaly
31.6719°
Eccentric anomaly
31.67974°
Mean motion
3.81392 °/min
Orbital period
94.39 mins
BSTAR
0.00049082
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-23 04:30:31.683Z | 108.927° ESE | 2025-11-23 04:32:31.683Z | 74.387° E | 16.324° | 2025-11-23 04:34:31.683Z | 35.636° NE |
| 4 mins | 2025-11-23 06:04:31.683Z | 221.56° SW | 2025-11-23 06:06:31.683Z | 273.847° WNW | 24.086° | 2025-11-23 06:08:31.683Z | 315.38° NNW |
| 4 mins | 2025-11-23 19:06:31.683Z | 321.935° NNW | 2025-11-23 19:07:31.683Z | 301.405° NW | 18.642° | 2025-11-23 19:10:31.683Z | 243.777° WSW |
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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