TAURUS R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite TAURUS R/B at a glance.

Uptime

9877

Days in orbit

Revolutions

≈ 14.7

Per day

Orbit

LEO

Low Earth Orbit

Inclination

85.1

Latest

Satellite identification and parameters

Extended collection of information and parameters for TAURUS R/B.

Object identification

Identified? True

Debris? False

Object name: TAURUS R/B

International designator: 1998-055B

Object number (NORAD): 25490

Object ID (CCSDS): 25490

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 97.867 minutes

Inclination: 85.0717 deg

SMA: 7034.776 km

Apoapsis: 666.629 km

Periapsis: 646.654 km

RAAN: 31.598 deg

Eccentricy: 0.00141972

Argument of periapsis: 346.5643 deg

Mean anomaly: 13.5191 deg

Mean motion: 14.71388458 rev/day

Mean motion (dot): 0.00000971 rev/day2

B* drag term: 0.00015271933 1/REarth

Two-line elements (TLE)

Creation date: Oct. 18, 2025, 2:17 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 17, 2025, 5:15 p.m. UTC

TLE line 0: 0 TAURUS R/B

TLE line 1: 1 25490U 98055B 25290.71943377 .00000971 00000-0 15272-3 0 9993

TLE line 2: 2 25490 85.0717 31.5980 0014197 346.5643 13.5191 14.71388458449296

Live tracking on map

Real-time ground track for satellite TAURUS R/B.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
CZ-4 DEB SSO 2025-06-26 16:48:26 0.0001318881 78.0 (m) DEBRIS
CZ-6A DEB SSO 2024-12-01 22:37:08 0.0001083909 372.0 (m) DEBRIS
SL-8 DEB * LEO 2024-11-15 18:06:11 0.0001610285 862.0 (m) DEBRIS
CZ-6A DEB SSO 2024-05-31 03:33:06 0.0001280146 464.0 (m) DEBRIS

Associated space launch

The STEX (Space Technology Experiments) satellite carried 29 new technologies intended to result in lower cost and higher performance spacecraft for future missions.

TAURUS R/B was lifted into orbit during the mission ‘Minotaur | NROL-8’, on board a Minotaur space rocket.

The launch took place on Oct. 3, 1998, 10:04 a.m. from Space Launch Complex 576E.

For more information about the launch, click the button.

Launch to space Minotaur | NROL-8
Minotaur | NROL-8

Agency: N/A

Status: Launch Successful

Launch date: Oct. 3, 1998, 10:04 a.m. UTC

Rocket: Minotaur

Launch pad: Space Launch Complex 576E

Location: Vandenberg SFB, CA, USA

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