FLOCK 4H 21, 66724
Orbit data source: Space-Track
FLOCK 4H 21, 66724 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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66724 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: 1 day ago
TLE from 1 day ago
0 FLOCK 4H 21
1 66724U 25276BL 26238.20668082 .00005817 00000-0 26148-3 0 9995
2 66724 97.4143 310.9142 0003933 77.3495 282.8181 15.21507289 40338Epoch: 2026-08-26T04:57Z
TLE epoch observation values (Epoch: 2026-08-26T04:57:37.222Z)
Latitude
0°
Longitude
-97.95389°
Altitude
503.786 km
Speed
7.613 km/s
True Right ascension
20h 43m 39s
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
22:33:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.962 km
Perigee altitude
495.553 km
Semi-major axis
6,876.395 km
Eccentricity
0.00039
Inclination
97.4143°
RAAN
310.9142°
Arg. of periapsis
77.3495°
True anomaly
282.77415°
Mean anomaly
282.8181°
Eccentric anomaly
282.79613°
Mean motion
3.80629 °/min
Orbital period
94.58 mins
BSTAR
0.00026148
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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 21 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 | 2026-08-27 17:49:30.222Z | 11.012° NNE | 2026-08-27 17:52:30.222Z | 250.675° W | 44.936° | 2026-08-27 17:55:30.222Z | 194.295° SSW |
| 5 mins | 2026-08-28 04:27:30.222Z | 127.154° SE | 2026-08-28 04:29:30.222Z | 79.228° E | 28.48° | 2026-08-28 04:32:30.222Z | 11.215° NNE |
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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