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
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 29
1 62642U 25009AK 26104.18237310 .00005156 00000-0 19035-3 0 9992
2 62642 97.4030 186.5009 0003975 144.0806 216.0702 15.28192520 69122Epoch: 2026-04-14T04:22Z
TLE epoch observation values (Epoch: 2026-04-14T04:22:37.035Z)
Latitude
0.00001°
Longitude
-81.51571°
Altitude
486.522 km
Speed
7.621 km/s
True Right ascension
12h 26m 00s
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
19:13:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.896 km
Perigee altitude
475.445 km
Semi-major axis
6,856.307 km
Eccentricity
0.0004
Inclination
97.403°
RAAN
186.5009°
Arg. of periapsis
144.0806°
True anomaly
216.04339°
Mean anomaly
216.0702°
Eccentric anomaly
216.05679°
Mean motion
3.82303 °/min
Orbital period
94.17 mins
BSTAR
0.00019035
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-14 17:31:44.985Z | 53.079° ENE | 2026-04-14 17:33:44.985Z | 92.6° ESE | 18.609° | 2026-04-14 17:35:44.985Z | 133.975° SE |
| 4 mins | 2026-04-14 19:05:44.985Z | 322.32° NNW | 2026-04-14 19:06:44.985Z | 299.912° NW | 20.155° | 2026-04-14 19:09:44.985Z | 239.583° WSW |
| 5 mins | 2026-04-15 05:39:44.985Z | 182.311° SSW | 2026-04-15 05:41:44.985Z | 267.339° W | 42.299° | 2026-04-15 05:44:44.985Z | 340.987° 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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