FLOCK 4BE 7, 60481
Orbit data source: Space-Track
FLOCK 4BE 7, 60481 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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60481 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 7
1 60481U 24149P 25301.45211204 .00018661 00000-0 62147-3 0 9994
2 60481 97.3983 18.8952 0003538 28.4407 331.7027 15.31166293 66683Epoch: 2025-10-28T10:51Z
TLE epoch observation values (Epoch: 2025-10-28T10:51:02.480Z)
Latitude
0.00002°
Longitude
179.09546°
Altitude
473.303 km
Speed
7.63 km/s
True Right ascension
01h 15m 34s
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
08:25:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.705 km
Perigee altitude
466.859 km
Semi-major axis
6,847.419 km
Eccentricity
0.00035
Inclination
97.3983°
RAAN
18.8952°
Arg. of periapsis
28.4407°
True anomaly
331.68347°
Mean anomaly
331.7027°
Eccentric anomaly
331.69309°
Mean motion
3.83048 °/min
Orbital period
93.98 mins
BSTAR
0.00062147
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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 7 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 | 2025-10-29 17:13:55.798Z | 58.028° ENE | 2025-10-29 17:15:55.798Z | 93.999° ESE | 14.69° | 2025-10-29 17:17:55.798Z | 129.651° SE |
| 4 mins | 2025-10-29 18:47:55.798Z | 322.624° NNW | 2025-10-29 18:48:55.798Z | 294.755° NW | 24.82° | 2025-10-29 18:51:55.798Z | 230.387° WSW |
| 5 mins | 2025-10-30 05:19:55.798Z | 166.237° S | 2025-10-30 05:21:55.798Z | 162.8° S | 42.475° | 2025-10-30 05:24:55.798Z | 348.644° 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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