FLOCK 4BE 8, 60515
Orbit data source: Space-Track
FLOCK 4BE 8, 60515 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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60515 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: 20 hours ago
TLE from 20 hours ago
0 FLOCK 4BE 8
1 60515U 24149AZ 25306.46280356 .00072563 00000-0 20409-2 0 9997
2 60515 97.3962 24.4597 0002631 350.0696 10.0495 15.36219192 67503Epoch: 2025-11-02T11:06Z
TLE epoch observation values (Epoch: 2025-11-02T11:06:26.227Z)
Latitude
-0.00008°
Longitude
175.87225°
Altitude
458.643 km
Speed
7.638 km/s
True Right ascension
01h 37m 50s
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
02:51:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.043 km
Perigee altitude
452.448 km
Semi-major axis
6,832.382 km
Eccentricity
0.00026
Inclination
97.3962°
RAAN
24.4597°
Arg. of periapsis
350.0696°
True anomaly
10.05476°
Mean anomaly
10.0495°
Eccentric anomaly
10.05213°
Mean motion
3.84313 °/min
Orbital period
93.67 mins
BSTAR
0.0020409
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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 8 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-03 17:23:09.586Z | 54.405° ENE | 2025-11-03 17:25:09.586Z | 93.33° ESE | 16.954° | 2025-11-03 17:27:09.586Z | 133.199° SE |
| 5 mins | 2025-11-04 05:27:09.586Z | 172.635° S | 2025-11-04 05:29:09.586Z | 249.275° W | 44.559° | 2025-11-04 05:32:09.586Z | 345.344° N |
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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