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: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4G 33
1 62685U 25009CE 26171.20012664 .00004610 00000-0 18492-3 0 9999
2 62685 97.3944 251.0360 0004284 332.0385 28.0622 15.25484482 79261Epoch: 2026-06-20T04:48Z
TLE epoch observation values (Epoch: 2026-06-20T04:48:10.941Z)
Latitude
-0.00007°
Longitude
-89.42774°
Altitude
489.833 km
Speed
7.622 km/s
True Right ascension
16h 44m 08s
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
10:19:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.23 km
Perigee altitude
483.348 km
Semi-major axis
6,864.426 km
Eccentricity
0.00043
Inclination
97.3944°
RAAN
251.036°
Arg. of periapsis
332.0385°
True anomaly
28.0853°
Mean anomaly
28.0622°
Eccentric anomaly
28.07375°
Mean motion
3.81625 °/min
Orbital period
94.33 mins
BSTAR
0.00018492
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 04:33:49.800Z | 115.117° SE | 2026-06-21 04:35:49.800Z | 80.116° E | 18.362° | 2026-06-21 04:38:49.800Z | 22.693° NE |
| 4 mins | 2026-06-21 06:07:49.800Z | 223.419° SW | 2026-06-21 06:09:49.800Z | 268.333° W | 21.116° | 2026-06-21 06:11:49.800Z | 309.701° NW |
| 4 mins | 2026-06-21 17:35:49.800Z | 52.728° ENE | 2026-06-21 17:37:49.800Z | 102.8° ESE | 24.051° | 2026-06-21 17:39:49.800Z | 146.336° SSE |
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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