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FLOCK 4BE 2, 60511

Orbit data source: Space-Track

FLOCK 4BE 2, 60511 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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/60511?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/60511?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60511, 2024-149AV

Orbit

SSO

Country

US

Related business

Planet Labs PBC (US)

Manufacturer

Planet

Mission

Non-operational Commercial Imaging

Bus & Motor

CUBESAT 3U, Unknown motor

Mass

5.7 kg wet, 5.7 kg dry

Launch date (UTC)

2024-08-16 (2 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

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 & history
Last TLE update: 7 hours ago

TLE from 7 hours ago

0 FLOCK 4BE 2
1 60511U 24149AV  26237.22048137  .00096081  00000-0  11158-2 0  9992
2 60511  97.3795 326.8987 0001827  34.3180 325.8195 15.61442100113243

Epoch: 2026-08-25T05:17Z

TLE epoch observation values (Epoch: 2026-08-25T05:17:29.590Z)

Latitude

-0.00005°

Longitude

-85.96554°

Altitude

385.616 km

Speed

7.679 km/s

True Right ascension

21h 47m 35s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

03:52:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

381.635 km

Perigee altitude

379.166 km

Semi-major axis

6,758.537 km

Eccentricity

0.00018

Inclination

97.3795°

RAAN

326.8987°

Arg. of periapsis

34.318°

True anomaly

325.80774°

Mean anomaly

325.8195°

Eccentric anomaly

325.81362°

Mean motion

3.90629 °/min

Orbital period

92.16 mins

BSTAR

0.0011158

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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)

SATELIOT_3, 60552

PTD-R (TYVAK-0127), 60523 (Decayed)

PICO-02E025, 60572 (Decayed)

FLOCK 4BE 35, 60558

PICO-02D024, 60569 (Decayed)

FLOCK 4BE 36, 60486

LEMU-NGE, 60532

FLOCK 4BE 3, 60561

FLOCK 4BE 15, 60491

NIGHTJAR, 60535

SATELIOT_4, 60537

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

FLOCK 4BE 2 Visibility

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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.
FLOCK 4BE 2 is likely not visible in the next few days.

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

Please sign in to view Co-orbital & Co-planar RSOs.

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out FLOCK 4BE 2, 60511 on other resources

View FLOCK 4BE 2, 60511 on NASA - NSSDCA Website

View FLOCK 4BE 2, 60511 on Heavens-Above

View FLOCK 4BE 2, 60511 on Keep Track

View FLOCK 4BE 2, 60511 on Celestrak

View FLOCK 4BE 2, 60511 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

Go to standalone docs website

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