FLOCK 4G 23, 62647
Orbit data source: Space-Track
FLOCK 4G 23, 62647 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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62647 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4G 23
1 62647U 25009AQ 26264.50541403 .00037316 00000-0 93055-3 0 9998
2 62647 97.3861 346.5846 0000564 248.6643 111.4543 15.40114388 93719Epoch: 2026-09-21T12:07Z
TLE epoch observation values (Epoch: 2026-09-21T12:07:47.772Z)
Latitude
0°
Longitude
164.25127°
Altitude
449.03 km
Speed
7.643 km/s
True Right ascension
23h 06m 20s
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
14:53:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.094 km
Perigee altitude
442.325 km
Semi-major axis
6,820.847 km
Eccentricity
0.00006
Inclination
97.3861°
RAAN
346.5846°
Arg. of periapsis
248.6643°
True anomaly
111.46031°
Mean anomaly
111.4543°
Eccentric anomaly
111.45731°
Mean motion
3.85288 °/min
Orbital period
93.44 mins
BSTAR
0.00093055
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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 23 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 | 2026-09-22 05:24:34.998Z | 153.027° SSE | 2026-09-22 05:27:34.998Z | 69.594° E | 56.444° | 2026-09-22 05:30:34.998Z | 357.547° N |
| 5 mins | 2026-09-22 18:19:34.998Z | 21.282° NNE | 2026-09-22 18:21:34.998Z | 76.564° E | 65.044° | 2026-09-22 18:24:34.998Z | 183.313° SSW |
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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