FLOCK 4G 29, 62642
Orbit data source: Space-Track
FLOCK 4G 29, 62642 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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62642 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 2 days ago
TLE from 2 days ago
0 FLOCK 4G 29
1 62642U 25009AK 26260.68788159 .00027706 00000-0 86070-3 0 9990
2 62642 97.3954 342.4046 0000969 294.4103 65.7038 15.33323223 93052Epoch: 2026-09-17T16:30Z
TLE epoch observation values (Epoch: 2026-09-17T16:30:32.969Z)
Latitude
-0.00003°
Longitude
98.1457°
Altitude
468.741 km
Speed
7.632 km/s
True Right ascension
22h 49m 37s
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
00:26:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.516 km
Perigee altitude
462.19 km
Semi-major axis
6,840.99 km
Eccentricity
0.0001
Inclination
97.3954°
RAAN
342.4046°
Arg. of periapsis
294.4103°
True anomaly
65.71392°
Mean anomaly
65.7038°
Eccentric anomaly
65.70886°
Mean motion
3.83588 °/min
Orbital period
93.85 mins
BSTAR
0.0008607
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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 29 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 | 2026-09-19 17:37:56.342Z | 47.443° ENE | 2026-09-19 17:40:56.342Z | 106.122° ESE | 18.85° | 2026-09-19 17:42:56.342Z | 141.6° SSE |
| 4 mins | 2026-09-19 19:11:56.342Z | 324.646° NNW | 2026-09-19 19:13:56.342Z | 276.968° WNW | 21.062° | 2026-09-19 19:15:56.342Z | 240.669° WSW |
| 5 mins | 2026-09-20 05:43:56.342Z | 178.608° S | 2026-09-20 05:45:56.342Z | 283.958° WNW | 69.966° | 2026-09-20 05:48:56.342Z | 343.212° N |
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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