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COSMOS 82, 1572

Orbit data source: Space-Track

COSMOS 82, 1572 is a payload satellite owned by OKB-10 (CIS) in LEO that was launched on Fri, 03 Sep 1965 UTC via a KOSMOS 65S3 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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/1572?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

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https://www.satcat.com/sats-embedded/1572?theme=dark&initialShowStats=false

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Identifier

1572, 1965-070C

Orbit

LEO

Last TLE update

2 days ago

Origin

Federal Space Agency of Russia (Roscosmos) (CIS)

Manufacturer

OKB-10

Mission

Defense Communications

Bus & Motor

STRELA-1 11F610, Unknown motor

Mass

50 kg wet, 50 kg dry

Launch date (UTC)

1965-09-03 (60 years ago)

Launch vehicle

KOSMOS 65S3

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Poly, 0.8 m

Radar Cross Section

0.731 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 2 days ago

0 COSMOS 82
1 01572U 65070C   25107.92693138 -.00000084  00000-0  70823-4 0  9996
2 01572  56.0596 314.8059 0076284  52.7532  61.8432 12.45116544711230

Epoch: 2025-04-17T22:14Z

Definitive object data (Epoch: 2025-04-17T22:14:46.871Z)

Latitude

48.68131°

Longitude

-94.80333°

Altitude

1,462.944 km

Speed

7.149 km/s

True Right ascension

05h 40m 44s

True Declination

48° 31' 34"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-12.6097°

Longitude

120.91199°

Altitude

1,468.098 km

Speed

7.138 km/s

Apparent Right ascension

18h 44m 19s

Apparent Declination

-26° 56' 53"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

04:36:19

Azimuth

286.226° WNW

Elevation

-60.528°

Doppler factor

Orbital elements

Apogee altitude

1,544.793 km

Perigee altitude

1,424.829 km

Semi-major axis

7,862.948 km

Eccentricity

0.0076284

Inclination

56.0596°

RAAN

314.8059°

Arg. of periapsis

52.7532°

True anomaly

62.61736°

Mean anomaly

61.8432°

Eccentric anomaly

62.22993°

Mean motion

3.1129 °/min

BSTAR

0.000070823

Orbital period

115.65 mins

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Other satellites on launch #70 in the year 1965 (1965-09-03 UTC)

COSMOS 82 Visibility forecast

Observer location: undefined°, undefined°

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.
16 mins	2025-04-19 22:18:49.850Z	319.358° NNW	2025-04-19 22:26:49.850Z	35.391° NE	39.144°	2025-04-19 22:34:49.850Z	110.161° ESE
15 mins	2025-04-20 00:20:49.850Z	302.56° NW	2025-04-20 00:27:49.850Z	232.065° WSW	37.291°	2025-04-20 00:35:49.850Z	164.684° S
7 mins	2025-04-20 13:21:49.850Z	133.864° SE	2025-04-20 13:24:49.850Z	111.526° ESE	14.45°	2025-04-20 13:28:49.850Z	82.998° E
15 mins	2025-04-20 15:16:49.850Z	209.595° SW	2025-04-20 15:23:49.850Z	143.964° SSE	43.128°	2025-04-20 15:31:49.850Z	49.662° ENE
14 mins	2025-04-20 17:18:49.850Z	267.147° W	2025-04-20 17:25:49.850Z	337.103° NNW	33.882°	2025-04-20 17:32:49.850Z	38.83° NE
13 mins	2025-04-20 19:22:49.850Z	309.485° NW	2025-04-20 19:28:49.850Z	0.333° NNE	24.641°	2025-04-20 19:35:49.850Z	54.688° ENE
14 mins	2025-04-20 21:25:49.850Z	325.533° NNW	2025-04-20 21:31:49.850Z	23.612° NE	33.194°	2025-04-20 21:39:49.850Z	93.964° ESE

Authenticating...

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Check out COSMOS 82, 1572 on other resources

View COSMOS 82, 1572 on NASA - NSSDCA Website

View COSMOS 82, 1572 on Heavens-Above

View COSMOS 82, 1572 on Keep Track

View COSMOS 82, 1572 on Celestrak

View COSMOS 82, 1572 on Gunter's Space Page

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