FLOCK 4G 10, 62670
Orbit data source: Space-Track
FLOCK 4G 10, 62670 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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62670 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
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 10
1 62670U 25009BP 26262.46384139 .00007742 00000-0 26056-3 0 9995
2 62670 97.3864 343.1344 0004119 20.9611 339.1798 15.31053052150951Epoch: 2026-09-19T11:07Z
TLE epoch observation values (Epoch: 2026-09-19T11:07:55.896Z)
Latitude
-0.00003°
Longitude
177.7795°
Altitude
473.137 km
Speed
7.631 km/s
True Right ascension
22h 52m 32s
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
09:03:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.44 km
Perigee altitude
466.799 km
Semi-major axis
6,847.756 km
Eccentricity
0.00041
Inclination
97.3864°
RAAN
343.1344°
Arg. of periapsis
20.9611°
True anomaly
339.16302°
Mean anomaly
339.1798°
Eccentric anomaly
339.17141°
Mean motion
3.83019 °/min
Orbital period
93.99 mins
BSTAR
0.00026056
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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 10 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 | 2026-09-19 17:58:30.614Z | 32.086° NE | 2026-09-19 18:01:30.614Z | 118.83° SE | 39.077° | 2026-09-19 18:03:30.614Z | 163.957° S |
| 5 mins | 2026-09-20 06:05:30.614Z | 211.561° SW | 2026-09-20 06:07:30.614Z | 263.636° W | 30.297° | 2026-09-20 06:10:30.614Z | 325.416° 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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