FLOCK 4BE 22, 60494
Orbit data source: Space-Track
FLOCK 4BE 22, 60494 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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60494 intel report (Beta)
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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: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4BE 22
1 60494U 24149AC 26264.97892881 .00027667 00000-0 59449-3 0 9997
2 60494 97.3681 349.6405 0002211 269.6310 90.4685 15.44646190117228Epoch: 2026-09-21T23:29Z
TLE epoch observation values (Epoch: 2026-09-21T23:29:39.449Z)
Latitude
-0.00003°
Longitude
-3.62486°
Altitude
435.555 km
Speed
7.65 km/s
True Right ascension
23h 18m 33s
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
11:58:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
430.854 km
Perigee altitude
427.844 km
Semi-major axis
6,807.486 km
Eccentricity
0.00022
Inclination
97.3681°
RAAN
349.6405°
Arg. of periapsis
269.631°
True anomaly
90.49384°
Mean anomaly
90.4685°
Eccentric anomaly
90.48117°
Mean motion
3.86423 °/min
Orbital period
93.16 mins
BSTAR
0.00059449
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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 22 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 | 2026-09-23 05:10:19.766Z | 126.594° SE | 2026-09-23 05:13:19.766Z | 59.857° ENE | 23.971° | 2026-09-23 05:15:19.766Z | 19.079° NNE |
| 4 mins | 2026-09-23 18:03:19.766Z | 56.489° ENE | 2026-09-23 18:04:19.766Z | 81.694° E | 24.819° | 2026-09-23 18:07:19.766Z | 152.679° 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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