ATLAS 2AS CENTAUR R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite ATLAS 2AS CENTAUR R/B at a glance.

Uptime

8703

Days in orbit

Revolutions

≈ 13.4

Per day

Orbit

LEO

Low Earth Orbit

Inclination

63.4

Latest

Satellite identification and parameters

Extended collection of information and parameters for ATLAS 2AS CENTAUR R/B.

Object identification

Identified? True

Debris? False

Object name: ATLAS 2AS CENTAUR R/B

International designator: 2001-040B

Object number (NORAD): 26906

Object ID (CCSDS): 26906

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 107.066 minutes

Inclination: 63.4271 deg

SMA: 7468.956 km

Apoapsis: 1538.145 km

Periapsis: 643.498 km

RAAN: 330.3883 deg

Eccentricy: 0.059891

Argument of periapsis: 340.8504 deg

Mean anomaly: 17.084 deg

Mean motion: 13.44970897 rev/day

Mean motion (dot): -0.00000051 rev/day2

B* drag term: 0.000027368 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 6:05 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 2:37 p.m. UTC

TLE line 0: 0 ATLAS 2AS CENTAUR R/B

TLE line 1: 1 26906U 01040B 25187.60936746 -.00000051 00000-0 27368-4 0 9999

TLE line 2: 2 26906 63.4271 330.3883 0598910 340.8504 17.0840 13.44970897 56926

Live tracking on map

Real-time ground track for satellite ATLAS 2AS CENTAUR R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object ATLAS 2AS CENTAUR R/B.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 1635 LEO 2025-01-10 03:44:36 0.0001264596 214.0 (m) PAYLOAD
DELTA 1 R/B(1) LEO 2024-10-29 16:50:17 0.0006530232 181.0 (m) ROCKET BODY
CZ-2D DEB SSO 2024-07-18 08:00:45 0.0002496571 715.0 (m) DEBRIS
CZ-6A DEB SSO 2024-06-28 00:17:47 0.0002181845 774.0 (m) DEBRIS

Associated space launch

NOSS-3 (Naval Ocean Surveillance System), which is likely not the official designation, is the third generation of NOSS satellites, which are low orbit SIGINT satellites. In 2013, the designation Intruder leaked out. These satellites carry equipment to track ships and aircraft via their radio transmissions. Positions of the origin of the transmissions are determined by triangulation. Each launch consists of two satellites of similar size in the same orbit. Both satellites maneuver to stationkeep relative to one another.

ATLAS 2AS CENTAUR R/B was lifted into orbit during the mission ‘Atlas IIAS | NROL-13’, on board a Atlas IIAS space rocket.

The launch took place on Sept. 8, 2001, 3:25 p.m. from Space Launch Complex 3E.

For more information about the launch, click the button.

Launch to space Atlas IIAS | NROL-13
Atlas IIAS | NROL-13

Agency: N/A

Status: Launch Successful

Launch date: Sept. 8, 2001, 3:25 p.m. UTC

Rocket: Atlas IIAS

Launch pad: Space Launch Complex 3E

Location: Vandenberg SFB, CA, USA

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