ATLAS CENTAUR R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite ATLAS CENTAUR R/B at a glance.

Uptime

20786

Days in orbit

Revolutions

≈ 14.6

Per day

Orbit

LEO

Low Earth Orbit

Inclination

35.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for ATLAS CENTAUR R/B.

Object identification

Identified? True

Debris? False

Object name: ATLAS CENTAUR R/B

International designator: 1968-110B

Object number (NORAD): 3598

Object ID (CCSDS): 3598

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 98.811 minutes

Inclination: 34.9933 deg

SMA: 7079.938 km

Apoapsis: 735.3 km

Periapsis: 668.306 km

RAAN: 316.7489 deg

Eccentricy: 0.0047313

Argument of periapsis: 239.8697 deg

Mean anomaly: 119.7303 deg

Mean motion: 14.57332262 rev/day

Mean motion (dot): 0.00000858 rev/day2

B* drag term: 0.0001882 1/REarth

Two-line elements (TLE)

Creation date: Nov. 2, 2025, 3:46 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Nov. 2, 2025, 10:35 a.m. UTC

TLE line 0: 0 ATLAS CENTAUR R/B

TLE line 1: 1 3598U 68110B 25306.44147818 .00000858 00000-0 18820-3 0 9997

TLE line 2: 2 3598 34.9933 316.7489 0047313 239.8697 119.7303 14.57332262991534

Live tracking on map

Real-time ground track for satellite ATLAS CENTAUR R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object ATLAS CENTAUR R/B.

Target Orbit TCA Probability of collision Miss distance Type
DMSP 5D-2 F13 DEB SSO 2025-10-13 08:25:47 0.0001030966 327.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-07-10 00:06:18 0.0001194054 250.0 (m) DEBRIS
CZ-2C DEB SSO 2025-01-04 02:32:01 0.0002700064 291.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-12-14 13:09:55 0.0003924212 158.0 (m) DEBRIS
NOAA 17 DEB SSO 2024-11-05 12:10:31 0.0001098631 761.0 (m) DEBRIS

Associated space launch

OAO 2 (Orbiting Astronomical Observatory), also known as Stargazer, was one of a series of automated astronomical observatories that was ground controllable in orientation and was placed in a low-earth orbit.

ATLAS CENTAUR R/B was lifted into orbit during the mission ‘Atlas SLV-3C Centaur | OAO 2’, on board a Atlas SLV-3C Centaur space rocket.

The launch took place on Dec. 7, 1968, 8:40 a.m. from Launch Complex 36B.

For more information about the launch, click the button.

Launch to space Atlas SLV-3C Centaur | OAO 2
Atlas SLV-3C Centaur | OAO 2

Agency: N/A

Status: Launch Successful

Launch date: Dec. 7, 1968, 8:40 a.m. UTC

Rocket: Atlas SLV-3C Centaur

Launch pad: Launch Complex 36B

Location: Cape Canaveral SFS, FL, USA

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