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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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: 22 hours ago
TLE from 22 hours ago
0 FLOCK 4G 23
1 62647U 25009AQ 25301.47805208 .00012883 00000-0 54029-3 0 9991
2 62647 97.4155 19.9891 0003375 84.6833 275.4789 15.23623197 43564Epoch: 2025-10-28T11:28Z
TLE epoch observation values (Epoch: 2025-10-28T11:28:23.699Z)
Latitude
-0.00005°
Longitude
170.82539°
Altitude
497.797 km
Speed
7.616 km/s
True Right ascension
01h 19m 57s
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
05:14:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.203 km
Perigee altitude
489.566 km
Semi-major axis
6,870.021 km
Eccentricity
0.00034
Inclination
97.4155°
RAAN
19.9891°
Arg. of periapsis
84.6833°
True anomaly
275.4404°
Mean anomaly
275.4789°
Eccentric anomaly
275.45965°
Mean motion
3.81159 °/min
Orbital period
94.45 mins
BSTAR
0.00054029
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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 | 2025-10-29 17:58:40.806Z | 21.865° NNE | 2025-10-29 18:01:40.806Z | 74.442° E | 38.165° | 2025-10-29 18:04:40.806Z | 174.896° S |
| 4 mins | 2025-10-30 06:10:40.806Z | 233.462° WSW | 2025-10-30 06:11:40.806Z | 256.134° W | 20.52° | 2025-10-30 06:14:40.806Z | 315.497° NNW |
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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