FLOCK 4G 17, 62681
Orbit data source: Space-Track
FLOCK 4G 17, 62681 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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62681 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: 1 day ago
TLE from 1 day ago
0 FLOCK 4G 17
1 62681U 25009CA 25300.21410205 .00012433 00000-0 52119-3 0 9998
2 62681 97.4144 18.5831 0006332 84.2031 275.9928 15.23632837101006Epoch: 2025-10-27T05:08Z
TLE epoch observation values (Epoch: 2025-10-27T05:08:18.417Z)
Latitude
0.00002°
Longitude
-94.3128°
Altitude
497.537 km
Speed
7.616 km/s
True Right ascension
01h 14m 19s
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
06:30:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.205 km
Perigee altitude
487.505 km
Semi-major axis
6,869.992 km
Eccentricity
0.00063
Inclination
97.4144°
RAAN
18.5831°
Arg. of periapsis
84.2031°
True anomaly
275.92063°
Mean anomaly
275.9928°
Eccentric anomaly
275.95672°
Mean motion
3.81161 °/min
Orbital period
94.45 mins
BSTAR
0.00052119
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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 17 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 | 2025-10-28 17:57:28.648Z | 25.705° NE | 2025-10-28 18:00:28.648Z | 118.346° SE | 37.866° | 2025-10-28 18:03:28.648Z | 176.778° S |
| 4 mins | 2025-10-29 06:08:28.648Z | 225.774° WSW | 2025-10-29 06:10:28.648Z | 272.206° WNW | 21.086° | 2025-10-29 06:12:28.648Z | 311.642° NW |
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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