FLOCK 4G 1, 62666
Orbit data source: Space-Track
FLOCK 4G 1, 62666 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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62666 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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4G 1
1 62666U 25009BK 26305.19330573 .00012435 00000-0 40115-3 0 9998
2 62666 97.3936 26.8090 0004314 172.0935 188.0375 15.32280759 99876Epoch: 2026-11-01T04:38Z
TLE epoch observation values (Epoch: 2026-11-01T04:38:21.615Z)
Latitude
-0.00006°
Longitude
-83.26925°
Altitude
475.042 km
Speed
7.627 km/s
True Right ascension
01h 47m 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
06:03:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.911 km
Perigee altitude
463.006 km
Semi-major axis
6,844.095 km
Eccentricity
0.00043
Inclination
97.3936°
RAAN
26.809°
Arg. of periapsis
172.0935°
True anomaly
188.03059°
Mean anomaly
188.0375°
Eccentric anomaly
188.03405°
Mean motion
3.83327 °/min
Orbital period
93.91 mins
BSTAR
0.00040115
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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 1 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 | 2026-11-01 17:44:43.698Z | 42.6° NE | 2026-11-01 17:47:43.698Z | 102.146° ESE | 22.087° | 2026-11-01 17:49:43.698Z | 142.657° SSE |
| 5 mins | 2026-11-02 05:51:43.698Z | 189.997° SSW | 2026-11-02 05:53:43.698Z | 293.435° NW | 54.297° | 2026-11-02 05:56:43.698Z | 340.17° N |
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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