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: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4G 11
1 62629U 25009W 26171.18289786 .00008721 00000-0 30851-3 0 9995
2 62629 97.3921 252.5964 0001378 336.1183 23.9993 15.29395428 79374Epoch: 2026-06-20T04:23Z
TLE epoch observation values (Epoch: 2026-06-20T04:23:22.375Z)
Latitude
-0.00001°
Longitude
-81.64801°
Altitude
479.859 km
Speed
7.626 km/s
True Right ascension
16h 50m 23s
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
07:23:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.515 km
Perigee altitude
473.627 km
Semi-major axis
6,852.708 km
Eccentricity
0.00014
Inclination
97.3921°
RAAN
252.5964°
Arg. of periapsis
336.1183°
True anomaly
24.00572°
Mean anomaly
23.9993°
Eccentric anomaly
24.00251°
Mean motion
3.82604 °/min
Orbital period
94.09 mins
BSTAR
0.00030851
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 05:37:59.866Z | 175.962° S | 2026-06-21 05:40:59.866Z | 229.755° WSW | 42.006° | 2026-06-21 05:43:59.866Z | 340.57° N |
| 5 mins | 2026-06-21 18:38:59.866Z | 348.818° N | 2026-06-21 18:40:59.866Z | 274.645° WNW | 36.383° | 2026-06-21 18:43:59.866Z | 211.649° SW |
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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