ATLAS CENTAUR 2 R/B, 694

Orbit data source: Space-Track

ATLAS CENTAUR 2 R/B, 694 is space debris in LEO originally from a launch on Wed, 27 Nov 1963 UTC via an ATLAS CENTAUR launch vehicle from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Iframe URL

https://www.satcat.com/sats-embedded/694?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

Identifier

694, 1963-047A

Orbit

LEO

Last TLE update

7 hours ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

GD/Convair

Mission

Civil Technology

Bus & Motor

AC R&D, Unknown motor

Mass

4,300 kg wet, 900 kg dry

Launch date (UTC)

1963-11-27 (62 years ago)

Launch vehicle

ATLAS CENTAUR

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 2 Nozzle, 4.3 m

Radar Cross Section

24.688 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 7 hours ago

0 ATLAS CENTAUR 2 R/B
1   694U 63047A   25199.02066832  .00001580  00000-0  18148-3 0  9991
2   694  30.3552  65.8584 0552442 174.1119 186.6312 14.10894362 98069

Epoch: 2025-07-18T00:29Z

TLE epoch observation values (Epoch: 2025-07-18T00:29:45.742Z)

Latitude

0.00001°

Longitude

122.3397°

Altitude

1,251.979 km

Speed

7.031 km/s

True Right ascension

04h 23m 26s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

21.90497°

Longitude

-102.45053°

Altitude

557.615 km

Speed

7.741 km/s

Apparent Right ascension

11h 24m 39s

Apparent Declination

-9° 10' 09"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

20:40:55

Azimuth

298.851° NW

Elevation

-42.398°

Doppler factor

Orbital elements

Apogee altitude

1,259.962 km

Perigee altitude

460.221 km

Semi-major axis

7,238.229 km

Eccentricity

0.05524

Inclination

30.3552°

RAAN

65.8584°

Arg. of periapsis

174.1119°

True anomaly

185.94721°

Mean anomaly

186.6312°

Eccentric anomaly

186.2847°

Mean motion

3.52448 °/min

Orbital period

102.14 mins

BSTAR

0.00018148

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Other satellites on launch #47 in the year 1963 (1963-11-27 UTC)

ATLAS CENTAUR 2 DEB, 696 (Decayed)

ATLAS CENTAUR 2 DEB, 697 (Decayed)

ATLAS CENTAUR 2 DEB, 698

ATLAS CENTAUR 2 DEB, 699 (Decayed)

ATLAS CENTAUR 2 DEB, 700

ATLAS CENTAUR 2 DEB, 701

ATLAS CENTAUR 2 DEB, 739

ATLAS CENTAUR 2 DEB, 1994 (Decayed)

ATLAS CENTAUR 2 DEB, 2886

ATLAS CENTAUR 2 DEB, 3741

ATLAS CENTAUR 2 DEB, 3922 (Decayed)

ATLAS CENTAUR 2 DEB, 6004 (Decayed)

ATLAS CENTAUR 2 DEB, 6158 (Decayed)

ATLAS CENTAUR 2 DEB, 19638

ATLAS CENTAUR 2 R/B 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.
7 mins	2025-07-18 17:39:51.657Z	185.437° SSW	2025-07-18 17:42:51.657Z	161.116° S	15.249°	2025-07-18 17:46:51.657Z	125.267° SE
9 mins	2025-07-18 19:26:51.657Z	217.88° SW	2025-07-18 19:31:51.657Z	162.581° S	25.323°	2025-07-18 19:35:51.657Z	116.501° SE
9 mins	2025-07-18 21:14:51.657Z	239.199° WSW	2025-07-18 21:19:51.657Z	175.225° S	27.632°	2025-07-18 21:23:51.657Z	123.528° SE
5 mins	2025-07-18 23:04:51.657Z	229.871° WSW	2025-07-18 23:06:51.657Z	202.251° SSW	18.98°	2025-07-18 23:09:51.657Z	158.351° S

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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Check out ATLAS CENTAUR 2 R/B, 694 on other resources

View ATLAS CENTAUR 2 R/B, 694 on Heavens-Above

View ATLAS CENTAUR 2 R/B, 694 on Keep Track

View ATLAS CENTAUR 2 R/B, 694 on Celestrak

View ATLAS CENTAUR 2 R/B, 694 on Gunter's Space Page

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