FLOCK 4G 33, 62685
Orbit data source: Space-Track
FLOCK 4G 33, 62685 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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62685 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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4G 33
1 62685U 25009CE 26126.19414589 .00005752 00000-0 23337-3 0 9991
2 62685 97.3945 206.5630 0007112 114.6186 245.5794 15.24981557 72402Epoch: 2026-05-06T04:39Z
TLE epoch observation values (Epoch: 2026-05-06T04:39:34.204Z)
Latitude
0.00001°
Longitude
-87.38766°
Altitude
495.961 km
Speed
7.616 km/s
True Right ascension
13h 46m 15s
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
21:21:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.683 km
Perigee altitude
482.916 km
Semi-major axis
6,865.937 km
Eccentricity
0.00071
Inclination
97.3945°
RAAN
206.563°
Arg. of periapsis
114.6186°
True anomaly
245.50522°
Mean anomaly
245.5794°
Eccentric anomaly
245.54231°
Mean motion
3.81499 °/min
Orbital period
94.36 mins
BSTAR
0.00023337
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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 33 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 | 2026-05-06 17:49:37.937Z | 31.435° NE | 2026-05-06 17:52:37.937Z | 115.682° SE | 32.902° | 2026-05-06 17:55:37.937Z | 170.762° S |
| 5 mins | 2026-05-07 05:59:37.937Z | 214.687° SW | 2026-05-07 06:01:37.937Z | 263.642° W | 25.345° | 2026-05-07 06:04:37.937Z | 323.384° NNW |
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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