FLOCK 4BE 25, 60487
Orbit data source: Space-Track
FLOCK 4BE 25, 60487 is a payload satellite owned by Planet (US) in SSO that was launched on Fri, 16 Aug 2024 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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60487 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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4BE 25
1 60487U 24149V 26035.14234649 .00018202 00000-0 54064-3 0 9999
2 60487 97.3899 117.7238 0002642 38.3419 321.8011 15.34830913 81803Epoch: 2026-02-04T03:24Z
TLE epoch observation values (Epoch: 2026-02-04T03:24:58.736Z)
Latitude
-0.0001°
Longitude
-67.83409°
Altitude
463.113 km
Speed
7.636 km/s
True Right ascension
07h 50m 53s
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
12:22:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.174 km
Perigee altitude
456.562 km
Semi-major axis
6,836.505 km
Eccentricity
0.00026
Inclination
97.3899°
RAAN
117.7238°
Arg. of periapsis
38.3419°
True anomaly
321.78237°
Mean anomaly
321.8011°
Eccentric anomaly
321.79174°
Mean motion
3.83965 °/min
Orbital period
93.76 mins
BSTAR
0.00054064
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Other satellites on launch #149 in the year 2024 (2024-08-16 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 4BE 25 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 | 2026-02-04 18:03:26.538Z | 21.526° NNE | 2026-02-04 18:06:26.538Z | 102.583° ESE | 40.301° | 2026-02-04 18:09:26.538Z | 179.5° S |
| 4 mins | 2026-02-05 06:09:26.538Z | 224.984° SW | 2026-02-05 06:11:26.538Z | 273.686° WNW | 20.731° | 2026-02-05 06:13:26.538Z | 313.428° NW |
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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