FLOCK 4G 2, 62661
Orbit data source: Space-Track
FLOCK 4G 2, 62661 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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62661 intel report (Beta)
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Edit Public Description
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: 16 hours ago
TLE from 16 hours ago
0 FLOCK 4G 2
1 62661U 25009BE 25286.47189622 .00017783 00000-0 75146-3 0 9991
2 62661 97.4232 5.3059 0006157 112.5176 247.6713 15.23280579 98889Epoch: 2025-10-13T11:19Z
TLE epoch observation values (Epoch: 2025-10-13T11:19:31.833Z)
Latitude
-0.00003°
Longitude
173.14907°
Altitude
500.658 km
Speed
7.613 km/s
True Right ascension
00h 21m 13s
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
21:23:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.146 km
Perigee altitude
488.685 km
Semi-major axis
6,871.053 km
Eccentricity
0.00062
Inclination
97.4232°
RAAN
5.3059°
Arg. of periapsis
112.5176°
True anomaly
247.60606°
Mean anomaly
247.6713°
Eccentric anomaly
247.63868°
Mean motion
3.81073 °/min
Orbital period
94.47 mins
BSTAR
0.00075146
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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 2 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 | 2025-10-14 04:48:15.738Z | 129.582° SE | 2025-10-14 04:51:15.738Z | 66.422° ENE | 25.497° | 2025-10-14 04:53:15.738Z | 21.024° NNE |
| 5 mins | 2025-10-14 17:51:15.738Z | 34.631° NE | 2025-10-14 17:53:15.738Z | 80.875° E | 32.367° | 2025-10-14 17:56:15.738Z | 164.985° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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