FLOCK 4H 7, 66710
Orbit data source: Space-Track
FLOCK 4H 7, 66710 is a payload satellite owned by Planet (US) in SSO that was launched on Fri, 28 Nov 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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66710 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: 15 hours ago
TLE from 15 hours ago
0 FLOCK 4H 7
1 66710U 25276AW 26238.67602209 .00007158 00000-0 32720-3 0 9993
2 66710 97.4145 311.0609 0003811 123.3608 236.7993 15.20848899 41130Epoch: 2026-08-26T16:13Z
TLE epoch observation values (Epoch: 2026-08-26T16:13:28.308Z)
Latitude
-0°
Longitude
92.76735°
Altitude
507.807 km
Speed
7.609 km/s
True Right ascension
20h 44m 14s
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
22:33:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.865 km
Perigee altitude
497.622 km
Semi-major axis
6,878.381 km
Eccentricity
0.00038
Inclination
97.4145°
RAAN
311.0609°
Arg. of periapsis
123.3608°
True anomaly
236.76277°
Mean anomaly
236.7993°
Eccentric anomaly
236.78103°
Mean motion
3.80464 °/min
Orbital period
94.62 mins
BSTAR
0.0003272
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Other satellites on launch #276 in the year 2025 (2025-11-28 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 4H 7 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-27 18:02:22.647Z | 2.152° NNE | 2026-08-27 18:06:22.647Z | 253.636° W | 37.097° | 2026-08-27 18:09:22.647Z | 207.993° SW |
| 5 mins | 2026-08-28 04:41:22.647Z | 142.254° SSE | 2026-08-28 04:43:22.647Z | 73.776° E | 38.446° | 2026-08-28 04:46:22.647Z | 0.33° 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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