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FLOCK 4G 4, 62659

Orbit data source: Space-Track

FLOCK 4G 4, 62659 is a payload satellite owned by Planet (US) in SSO that was launched on Tue, 14 Jan 2025 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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<iframe src="https://www.satcat.com/sats-embedded/62659?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/62659?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

62659, 2025-009BC

Orbit

SSO

Country

US

Related business

Planet Labs PBC (US)

Manufacturer

Planet

Mission

Partially operational Commercial Imaging

Bus & Motor

CUBESAT 3U, Unknown motor

Mass

5.7 kg wet, 5.7 kg dry

Launch date (UTC)

2025-01-14 (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: 2 days ago

TLE from 2 days ago

0 FLOCK 4G 4
1 62659U 25009BC  26215.19179172  .00041340  00000-0  12740-2 0  9995
2 62659  97.3923 296.4115 0004953 143.7059 216.4521 15.33480987143705

Epoch: 2026-08-03T04:36Z

TLE epoch observation values (Epoch: 2026-08-03T04:36:10.804Z)

Latitude

0.00004°

Longitude

-84.41196°

Altitude

471.273 km

Speed

7.629 km/s

True Right ascension

19h 45m 38s

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

19:53:09

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

465.772 km

Perigee altitude

458.995 km

Semi-major axis

6,840.52 km

Eccentricity

0.0005

Inclination

97.3923°

RAAN

296.4115°

Arg. of periapsis

143.7059°

True anomaly

216.41839°

Mean anomaly

216.4521°

Eccentric anomaly

216.43525°

Mean motion

3.83627 °/min

Orbital period

93.84 mins

BSTAR

0.001274

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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)

HYPE, 62687 (Decayed)

OBJECT DM, 63002 (Decayed)

OBJECT F, 62614 (Decayed)

EDISON-1, 62610

FLOCK 4G 2, 62661

FLOCK 4G 10, 62670

SKYBEE-A01, 62671

FLOCK 4G 30, 62679

FLOCK 4G 33, 62685

FOSSASAT2E20 (TAT-O), 63003

FLOCK 4G 12, 62625

FLOCK 4G 3, 62639

FLOCK 4G 5, 62663

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 4G 4 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.
6 mins	2026-08-05 18:14:24.855Z	18.248° NNE	2026-08-05 18:17:24.855Z	149.122° SSE	41.671°	2026-08-05 18:20:24.855Z	186.149° SSW

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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 4G 4, 62659 on other resources

View FLOCK 4G 4, 62659 on NASA - NSSDCA Website

View FLOCK 4G 4, 62659 on Heavens-Above

View FLOCK 4G 4, 62659 on Keep Track

View FLOCK 4G 4, 62659 on Celestrak

View FLOCK 4G 4, 62659 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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