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GOES 2, 10061

Orbit data source: Space-Track

GOES 2, 10061 is a payload satellite owned by NOAA (US) in GEO that was launched on Thu, 16 Jun 1977 UTC via a DELTA 2914 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.

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Iframe URL

https://www.satcat.com/sats-embedded/10061?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

10061, 1977-048A

Orbit

GEO

Country

Related business

National Oceanic and Atmospheric Administration (US)

Manufacturer

Ford Ae

Mission

Non-operational spacecraft

Bus & Motor

SMS, SVM-5

Mass

624 kg wet, ~277 kg dry

Launch date (UTC)

1977-06-16 (48 years ago)

Launch vehicle

DELTA 2914

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

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Last TLE update: 14 hours ago

TLE from 14 hours ago

0 GOES 2
1 10061U 77048A   25290.23562252 -.00000064  00000-0  00000-0 0  9990
2 10061   7.0024 295.3572 0011148  40.2995 325.3735  0.99400591 43866

Epoch: 2025-10-17T05:39Z

TLE epoch observation values (Epoch: 2025-10-17T05:39:17.785Z)

Latitude

0.70269°

Longitude

-169.90135°

Altitude

35,993.242 km

Speed

3.069 km/s

True Right ascension

20h 03m 37s

True Declination

0° 42' 07"

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

14:48:45

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

36,080.926 km

Perigee altitude

35,986.365 km

Semi-major axis

42,411.783 km

Eccentricity

0.00111

Inclination

7.0024°

RAAN

295.3572°

Arg. of periapsis

40.2995°

True anomaly

325.30083°

Mean anomaly

325.3735°

Eccentric anomaly

325.33717°

Mean motion

0.24849 °/min

Orbital period

1,448.74 mins

BSTAR

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Other satellites on launch #48 in the year 1977 (1977-06-16 UTC)

DELTA 1 R/B(1), 10062

GOES 2 AKM, 20799

DELTA 1 DEB, 10063 (Decayed)

DELTA 1 DEB, 10067 (Decayed)

DELTA 1 R/B(2), 10409 (Decayed)

DELTA 1 DEB, 10075 (Decayed)

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GOES 2 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.
480 mins	2025-10-18 07:14:55.363Z	258.158° W	2025-10-18 11:27:55.363Z	261.37° W	12.224°	2025-10-18 15:14:55.363Z	258.991° W

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10061 neighbors

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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 GOES 2, 10061 on other resources

View GOES 2, 10061 on NASA - NSSDCA Website

View GOES 2, 10061 on Heavens-Above

View GOES 2, 10061 on Keep Track

View GOES 2, 10061 on Celestrak

View GOES 2, 10061 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

GOES 2, 10061

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2025-10-17T05:39:17.785Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #48 in the year 1977 (1977-06-16 UTC)

GOES 2 Visibility forecast

10061 neighbors

Co-orbital & Co-planar RSOs

Check out GOES 2, 10061 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago