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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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/60481?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/60481?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60481, 2024-149P

Orbit

SSO

Country

US

Related business

Planet Labs PBC (US)

Manufacturer

Planet

Mission

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: 15 hours ago

TLE from 15 hours ago

0 FLOCK 4BE 7
1 60481U 24149P   26260.22729656  .00032017  00000-0  69793-3 0  9994
2 60481  97.3698 344.2999 0001453 287.3696  72.7393 15.44191624116430

Epoch: 2026-09-17T05:27Z

TLE epoch observation values (Epoch: 2026-09-17T05:27:18.422Z)

Latitude

-0.00008°

Longitude

-93.69441°

Altitude

436.585 km

Speed

7.65 km/s

True Right ascension

22h 57m 11s

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

13:18:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

431.676 km

Perigee altitude

429.697 km

Semi-major axis

6,808.823 km

Eccentricity

0.00015

Inclination

97.3698°

RAAN

344.2999°

Arg. of periapsis

287.3696°

True anomaly

72.7552°

Mean anomaly

72.7393°

Eccentric anomaly

72.74725°

Mean motion

3.86309 °/min

Orbital period

93.19 mins

BSTAR

0.00069793

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

PICO-02C023, 60564 (Decayed)

NIGHTJAR, 60535

TROOP-F2, 60557 (Decayed)

LEMU-NGE, 60532

EAGLEEYE, 60508

TANAGER-1 4001, 60507

FLOCK 4BE 11, 60501

FLOCK 4BE 33, 60502 (Decayed)

FLOCK 4BE 23, 60490

PICO-02F026, 60567 (Decayed)

SATELIOT_2, 60534

FLOCK 4BE 5, 60559

HAWK-10B, 60545

PICO-02A021, 60538

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 7 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 7 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

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

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Check out FLOCK 4BE 7, 60481 on other resources

View FLOCK 4BE 7, 60481 on NASA - NSSDCA Website

View FLOCK 4BE 7, 60481 on Heavens-Above

View FLOCK 4BE 7, 60481 on Keep Track

View FLOCK 4BE 7, 60481 on Celestrak

View FLOCK 4BE 7, 60481 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

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