FLOCK 4BE 15, 60491
Orbit data source: Space-Track
FLOCK 4BE 15, 60491 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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60491 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: 12 hours ago
TLE from 12 hours ago
0 FLOCK 4BE 15
1 60491U 24149Z 25300.46834390 .00016311 00000-0 50217-3 0 9997
2 60491 97.3941 18.0829 0004553 61.9851 298.1852 15.33711647 66566Epoch: 2025-10-27T11:14Z
TLE epoch observation values (Epoch: 2025-10-27T11:14:24.912Z)
Latitude
-0.00003°
Longitude
173.40935°
Altitude
466.388 km
Speed
7.634 km/s
True Right ascension
01h 12m 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
19:04:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.811 km
Perigee altitude
458.583 km
Semi-major axis
6,839.834 km
Eccentricity
0.00046
Inclination
97.3941°
RAAN
18.0829°
Arg. of periapsis
61.9851°
True anomaly
298.1392°
Mean anomaly
298.1852°
Eccentric anomaly
298.1622°
Mean motion
3.83685 °/min
Orbital period
93.83 mins
BSTAR
0.00050217
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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 15 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 | 2025-10-28 04:37:03.958Z | 111.784° ESE | 2025-10-28 04:39:03.958Z | 67.605° E | 20.059° | 2025-10-28 04:41:03.958Z | 25.932° NE |
| 4 mins | 2025-10-28 17:35:03.958Z | 65.703° ENE | 2025-10-28 17:36:03.958Z | 93.7° ESE | 23.62° | 2025-10-28 17:39:03.958Z | 154.991° 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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