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: 5 hours ago
TLE from 5 hours ago
0 FLOCK 4G 33
1 62685U 25009CE 26262.47762178 .00003898 00000-0 15234-3 0 9999
2 62685 97.3887 341.3015 0005370 14.1515 345.9873 15.26446657 93186Epoch: 2026-09-19T11:27Z
TLE epoch observation values (Epoch: 2026-09-19T11:27:46.521Z)
Latitude
-0.00005°
Longitude
170.97208°
Altitude
485.967 km
Speed
7.624 km/s
True Right ascension
22h 45m 12s
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
09:02:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.086 km
Perigee altitude
479.717 km
Semi-major axis
6,861.538 km
Eccentricity
0.00054
Inclination
97.3887°
RAAN
341.3015°
Arg. of periapsis
14.1515°
True anomaly
345.97239°
Mean anomaly
345.9873°
Eccentric anomaly
345.97985°
Mean motion
3.81866 °/min
Orbital period
94.27 mins
BSTAR
0.00015234
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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 | 2026-09-19 18:18:42.416Z | 8.372° NNE | 2026-09-19 18:21:42.416Z | 322.733° NNW | 73.399° | 2026-09-19 18:24:42.416Z | 198.62° SSW |
| 4 mins | 2026-09-20 04:55:42.416Z | 114.768° SE | 2026-09-20 04:56:42.416Z | 85.432° E | 32.962° | 2026-09-20 04:59:42.416Z | 11.755° NNE |
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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