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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4G 11
1 62629U 25009W 26079.52829607 .00009483 00000-0 35555-3 0 9994
2 62629 97.3957 161.5973 0001418 257.1229 102.9852 15.27459095 65376Epoch: 2026-03-20T12:40Z
TLE epoch observation values (Epoch: 2026-03-20T12:40:44.780Z)
Latitude
-0.00001°
Longitude
153.34865°
Altitude
486.731 km
Speed
7.622 km/s
True Right ascension
10h 46m 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
15:55:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.339 km
Perigee altitude
479.394 km
Semi-major axis
6,858.504 km
Eccentricity
0.00014
Inclination
97.3957°
RAAN
161.5973°
Arg. of periapsis
257.1229°
True anomaly
103.00103°
Mean anomaly
102.9852°
Eccentric anomaly
102.99312°
Mean motion
3.82119 °/min
Orbital period
94.21 mins
BSTAR
0.00035555
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-21 17:33:17.452Z | 47.184° ENE | 2026-03-21 17:35:17.452Z | 85.205° E | 20.528° | 2026-03-21 17:38:17.452Z | 146.395° SSE |
| 5 mins | 2026-03-22 05:42:17.452Z | 193.786° SSW | 2026-03-22 05:44:17.452Z | 293.879° NW | 37.824° | 2026-03-22 05:47:17.452Z | 339.245° N |
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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