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TUSUR GO, 61782

Orbit data source: Space-Track

TUSUR GO, 61782 is a Commonwealth of Independent States-origin payload satellite in LEO that was launched on Mon, 04 Nov 2024 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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/61782?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/61782?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

61782, 2024-199AZ

Orbit

LEO

Country

CIS

Related business

Tomsk State U. of Control Systems and Radioelectronics (RU)

Manufacturer

Geoskan

Mission

Operational Amateur Technology

Bus & Motor

CUBESAT 3U, Unknown motor

Mass

5 kg wet, 5 kg dry

Launch date (UTC)

2024-11-04 (2 years ago)

Launch vehicle

SOYUZ-2-1B

Launch site

Vostochny Cosmodrome (VOSTO)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 0.1 m

Radar Cross Section

0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 TUSUR GO
1 61782U 24199AZ  26126.92283649  .06698914  24578-5  11300-2 0  9990
2 61782  97.2729   8.6700 0008386 236.8511 123.1981 16.33156919128453

Epoch: 2026-05-06T22:08Z

TLE epoch observation values (Epoch: 2026-05-06T22:08:53.072Z)

Latitude

-0.00006°

Longitude

171.6725°

Altitude

190.333 km

Speed

7.79 km/s

True Right ascension

00h 34m 40s

True Declination

0° 00' 00"

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

16:39:47

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

186.381 km

Perigee altitude

175.38 km

Semi-major axis

6,559.017 km

Eccentricity

0.00084

Inclination

97.2729°

RAAN

8.67°

Arg. of periapsis

236.8511°

True anomaly

123.27847°

Mean anomaly

123.1981°

Eccentric anomaly

123.23829°

Mean motion

4.08587 °/min

Orbital period

88.11 mins

BSTAR

0.00113

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Other satellites on launch #199 in the year 2024 (2024-11-04 UTC)

OBJECT K, 61744

OBJECT AC, 61761

OBJECT T, 61752

IONOSFERA-M 02, 61736

OBJECT AL, 61769

OBJECT H, 61742

OBJECT BD, 61786

OBJECT E, 61739

OBJECT Z, 61758

OBJECT BF, 61788

OBJECT AT, 61776

OBJECT AU, 61777

ARCTICSAT-1, 61762

OBJECT AS, 61775

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

TUSUR GO 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.
TUSUR GO 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 TUSUR GO, 61782 on other resources

View TUSUR GO, 61782 on NASA - NSSDCA Website

View TUSUR GO, 61782 on Heavens-Above

View TUSUR GO, 61782 on Keep Track

View TUSUR GO, 61782 on Celestrak

View TUSUR GO, 61782 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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