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STARLINK-36996, 68064

Orbit data source: Space-Track

STARLINK-36996, 68064 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 02 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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

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Iframe URL

https://www.satcat.com/sats-embedded/68064?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

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ISO8601 Format

Identifier

68064, 2026-041AA

Orbit

LEO

Country

US

Related business

Manufacturer

SpaceX/Seattle

Mission

Operational spacecraft

Bus & Motor

STARLINK V2MO, Unknown motor

Mass

575 kg wet, ~530 kg dry

Launch date (UTC)

2026-03-02 (6 days ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

RCS unknown

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago

0 STARLINK-36996
1 68064U 26041AA  26066.58334491 -.01394525  61317-3 -25441-2 0  9994
2 68064  53.1591  72.9781 0000555  64.0998 208.1653 16.00790097  2034

Epoch: 2026-03-07T14:00Z

TLE epoch observation values (Epoch: 2026-03-07T14:00:01.000Z)

Latitude

-53.25588°

Longitude

-28.56893°

Altitude

291.041 km

Speed

7.732 km/s

True Right ascension

23h 06m 57s

True Declination

-53° 04' 45"

Sunlit

Object was in daylight 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

04:58:30

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

272.863 km

Perigee altitude

272.125 km

Semi-major axis

6,650.631 km

Eccentricity

0.00006

Inclination

53.1591°

RAAN

72.9781°

Arg. of periapsis

64.0998°

True anomaly

208.1623°

Mean anomaly

208.1653°

Eccentric anomaly

208.1638°

Mean motion

4.00174 °/min

Orbital period

89.96 mins

BSTAR

-0.0025441

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Computing Atmospheric mass density...

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Other satellites on launch #41 in the year 2026 (2026-03-02 UTC)

STARLINK-36952, 68062

STARLINK-35808, 68052

STARLINK-36825, 68041

STARLINK-36864, 68045

STARLINK-35911, 68051

STARLINK-36924, 68054

STARLINK-36711, 68040

STARLINK-36318, 68048

STARLINK-36899, 68058

STARLINK-36836, 68065

STARLINK-37000, 68063

STARLINK-36845, 68056

STARLINK-36915, 68061

STARLINK-36181, 68047

STARLINK-36966, 68044

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

STARLINK-36996 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.
STARLINK-36996 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

Authenticating...

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Check out STARLINK-36996, 68064 on other resources

View STARLINK-36996, 68064 on NASA - NSSDCA Website

View STARLINK-36996, 68064 on Heavens-Above

View STARLINK-36996, 68064 on Keep Track

View STARLINK-36996, 68064 on Celestrak

View STARLINK-36996, 68064 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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