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: 1 day ago
TLE from 1 day ago
0 FLOCK 4BE 25
1 60487U 24149V 25301.18286844 .00017221 00000-0 57808-3 0 9991
2 60487 97.4011 18.7692 0002897 34.0109 326.1317 15.30929965 66649Epoch: 2025-10-28T04:23Z
TLE epoch observation values (Epoch: 2025-10-28T04:23:19.833Z)
Latitude
-0.00004°
Longitude
-83.83746°
Altitude
474.493 km
Speed
7.63 km/s
True Right ascension
01h 15m 04s
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
05:25:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.971 km
Perigee altitude
468.004 km
Semi-major axis
6,848.124 km
Eccentricity
0.00029
Inclination
97.4011°
RAAN
18.7692°
Arg. of periapsis
34.0109°
True anomaly
326.11319°
Mean anomaly
326.1317°
Eccentric anomaly
326.12245°
Mean motion
3.82988 °/min
Orbital period
94 mins
BSTAR
0.00057808
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-29 18:36:06.538Z | 348.035° N | 2025-10-29 18:38:06.538Z | 298.142° NW | 31.762° | 2025-10-29 18:41:06.538Z | 220.369° SW |
| 4 mins | 2025-10-30 05:10:06.538Z | 144.828° SSE | 2025-10-30 05:12:06.538Z | 38.275° NE | 38.87° | 2025-10-30 05:14:06.538Z | 359.358° N |
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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