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: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4G 33
1 62685U 25009CE 26307.17873346 .00004212 00000-0 16215-3 0 9997
2 62685 97.3855 25.5164 0005244 182.2013 177.9204 15.26905774100008Epoch: 2026-11-03T04:17Z
TLE epoch observation values (Epoch: 2026-11-03T04:17:22.570Z)
Latitude
-0.00003°
Longitude
-81.27276°
Altitude
491.766 km
Speed
7.617 km/s
True Right ascension
01h 42m 03s
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
14:44:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.622 km
Perigee altitude
478.427 km
Semi-major axis
6,860.161 km
Eccentricity
0.00052
Inclination
97.3855°
RAAN
25.5164°
Arg. of periapsis
182.2013°
True anomaly
177.92258°
Mean anomaly
177.9204°
Eccentric anomaly
177.92149°
Mean motion
3.81981 °/min
Orbital period
94.25 mins
BSTAR
0.00016215
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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 | 2026-11-03 18:59:58.120Z | 341° N | 2026-11-03 19:02:58.120Z | 282.345° WNW | 22.109° | 2026-11-03 19:04:58.120Z | 243.411° WSW |
| 5 mins | 2026-11-04 05:35:58.120Z | 184.196° SSW | 2026-11-04 05:37:58.120Z | 288.275° WNW | 62.668° | 2026-11-04 05:40:58.120Z | 341.44° N |
| 5 mins | 2026-11-04 18:36:58.120Z | 343.218° N | 2026-11-04 18:38:58.120Z | 265.185° W | 42.761° | 2026-11-04 18:41:58.120Z | 212.869° 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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