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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Edit Public Description
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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4G 29
1 62642U 25009AK 25261.16591881 .00009919 00000-0 43433-3 0 9999
2 62642 97.4268 340.3353 0004105 153.9878 206.1565 15.22222974 37416Epoch: 2025-09-18T03:58Z
TLE epoch observation values (Epoch: 2025-09-18T03:58:55.385Z)
Latitude
-0.00003°
Longitude
-76.72689°
Altitude
504.765 km
Speed
7.61 km/s
True Right ascension
22h 41m 20s
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
11:20:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.923 km
Perigee altitude
493.279 km
Semi-major axis
6,874.238 km
Eccentricity
0.00041
Inclination
97.4268°
RAAN
340.3353°
Arg. of periapsis
153.9878°
True anomaly
206.13577°
Mean anomaly
206.1565°
Eccentric anomaly
206.14614°
Mean motion
3.80808 °/min
Orbital period
94.54 mins
BSTAR
0.00043433
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 18:44:24.439Z | 349.432° N | 2025-09-18 18:47:24.439Z | 277.531° WNW | 29.477° | 2025-09-18 18:50:24.439Z | 221.362° SW |
| 5 mins | 2025-09-19 05:22:24.439Z | 160.892° S | 2025-09-19 05:24:24.439Z | 13.792° NNE | 43.37° | 2025-09-19 05:27:24.439Z | 350.377° N |
| 4 mins | 2025-09-19 18:25:24.439Z | 359.525° N | 2025-09-19 18:27:24.439Z | 270.796° WNW | 42.227° | 2025-09-19 18:29:24.439Z | 207.136° 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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