FLOCK 4G 6, 62660
Orbit data source: Space-Track
FLOCK 4G 6, 62660 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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62660 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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4G 6
1 62660U 25009BD 26171.48528959 .00007479 00000-0 26366-3 0 9996
2 62660 97.3938 252.8850 0002110 340.3955 19.7204 15.29559186137009Epoch: 2026-06-20T11:38Z
TLE epoch observation values (Epoch: 2026-06-20T11:38:49.020Z)
Latitude
-0.00002°
Longitude
169.48152°
Altitude
478.871 km
Speed
7.627 km/s
True Right ascension
16h 51m 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
07:23:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.527 km
Perigee altitude
472.636 km
Semi-major axis
6,852.219 km
Eccentricity
0.00021
Inclination
97.3938°
RAAN
252.885°
Arg. of periapsis
340.3955°
True anomaly
19.72856°
Mean anomaly
19.7204°
Eccentric anomaly
19.72448°
Mean motion
3.82645 °/min
Orbital period
94.08 mins
BSTAR
0.00026366
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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 6 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 | 2026-06-21 05:02:43.791Z | 141.251° SSE | 2026-06-21 05:05:43.791Z | 81.801° E | 30.994° | 2026-06-21 05:08:43.791Z | 8.055° NNE |
| 5 mins | 2026-06-21 18:03:43.791Z | 35.863° NE | 2026-06-21 18:05:43.791Z | 122.102° SE | 36.907° | 2026-06-21 18:08:43.791Z | 176.636° S |
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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