FLOCK 4G 11, 62629
Orbit data source: Space-Track
FLOCK 4G 11, 62629 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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62629 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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4G 11
1 62629U 25009W 26253.44854683 .00009447 00000-0 31843-3 0 9997
2 62629 97.3882 334.4485 0003228 46.8071 313.3439 15.30942627 91955Epoch: 2026-09-10T10:45Z
TLE epoch observation values (Epoch: 2026-09-10T10:45:54.446Z)
Latitude
-0.00003°
Longitude
-176.51446°
Altitude
474.586 km
Speed
7.629 km/s
True Right ascension
22h 17m 47s
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
11:10:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.16 km
Perigee altitude
467.739 km
Semi-major axis
6,848.086 km
Eccentricity
0.00032
Inclination
97.3882°
RAAN
334.4485°
Arg. of periapsis
46.8071°
True anomaly
313.31699°
Mean anomaly
313.3439°
Eccentric anomaly
313.33045°
Mean motion
3.82992 °/min
Orbital period
94 mins
BSTAR
0.00031843
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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 11 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 | 2026-09-10 19:10:02.808Z | 335.336° NNW | 2026-09-10 19:12:02.808Z | 297.412° NW | 20.539° | 2026-09-10 19:14:02.808Z | 253.185° W |
| 5 mins | 2026-09-11 05:44:02.808Z | 185.416° SSW | 2026-09-11 05:46:02.808Z | 292.193° WNW | 59.766° | 2026-09-11 05:49:02.808Z | 341.337° N |
| 4 mins | 2026-09-11 18:43:02.808Z | 343.38° N | 2026-09-11 18:45:02.808Z | 258.258° W | 43.115° | 2026-09-11 18:47:02.808Z | 216.528° SW |
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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