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: 2 days ago
TLE from 2 days ago
0 FLOCK 4G 33
1 62685U 25009CE 26215.73101541 .00006211 00000-0 24414-3 0 9999
2 62685 97.3925 295.0692 0006466 149.0621 211.0999 15.26012437 86053Epoch: 2026-08-03T17:32Z
TLE epoch observation values (Epoch: 2026-08-03T17:32:39.731Z)
Latitude
-0.00007°
Longitude
79.59374°
Altitude
494.649 km
Speed
7.615 km/s
True Right ascension
19h 40m 16s
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
20:48:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.142 km
Perigee altitude
480.267 km
Semi-major axis
6,862.841 km
Eccentricity
0.00065
Inclination
97.3925°
RAAN
295.0692°
Arg. of periapsis
149.0621°
True anomaly
211.06165°
Mean anomaly
211.0999°
Eccentric anomaly
211.08077°
Mean motion
3.81757 °/min
Orbital period
94.3 mins
BSTAR
0.00024414
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-05 17:20:23.063Z | 57.238° ENE | 2026-08-05 17:22:23.063Z | 94.664° ESE | 16.192° | 2026-08-05 17:24:23.063Z | 131.603° SE |
| 4 mins | 2026-08-05 18:54:23.063Z | 326.349° NNW | 2026-08-05 18:55:23.063Z | 302.548° NW | 22.959° | 2026-08-05 18:58:23.063Z | 235.811° WSW |
| 5 mins | 2026-08-06 05:29:23.063Z | 174.822° S | 2026-08-06 05:31:23.063Z | 289.087° WNW | 44.148° | 2026-08-06 05:34:23.063Z | 344.749° 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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