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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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: 17 hours ago
TLE from 17 hours ago
0 FLOCK 4G 17
1 62681U 25009CA 26171.20778928 .00008217 00000-0 28909-3 0 9998
2 62681 97.3919 252.5650 0003450 335.0589 25.0484 15.29594053137011Epoch: 2026-06-20T04:59Z
TLE epoch observation values (Epoch: 2026-06-20T04:59:12.993Z)
Latitude
-0.00006°
Longitude
-90.66485°
Altitude
477.986 km
Speed
7.628 km/s
True Right ascension
16h 50m 15s
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
08:42:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.341 km
Perigee altitude
471.613 km
Semi-major axis
6,852.114 km
Eccentricity
0.00035
Inclination
97.3919°
RAAN
252.565°
Arg. of periapsis
335.0589°
True anomaly
25.06514°
Mean anomaly
25.0484°
Eccentric anomaly
25.05677°
Mean motion
3.82654 °/min
Orbital period
94.08 mins
BSTAR
0.00028909
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 04:40:59.732Z | 116.134° SE | 2026-06-21 04:42:59.732Z | 80.87° E | 18.345° | 2026-06-21 04:45:59.732Z | 22.362° NNE |
| 4 mins | 2026-06-21 06:14:59.732Z | 227.646° WSW | 2026-06-21 06:16:59.732Z | 274.149° WNW | 20.001° | 2026-06-21 06:18:59.732Z | 312.278° NW |
| 4 mins | 2026-06-21 17:40:59.732Z | 54.332° ENE | 2026-06-21 17:42:59.732Z | 104.432° ESE | 22.926° | 2026-06-21 17:44:59.732Z | 146.366° SSE |
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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