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

7663

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

99.1

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: 2004-018B

Object number (NORAD): 28255

Object ID (CCSDS): 28255

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.191 minutes

Inclination: 99.0954 deg

SMA: 7098.106 km

Apoapsis: 730.477 km

Periapsis: 709.466 km

RAAN: 199.1339 deg

Eccentricy: 0.00148

Argument of periapsis: 64.3039 deg

Mean anomaly: 295.968 deg

Mean motion: 14.51740554 rev/day

Mean motion (dot): 0.00000298 rev/day2

B* drag term: 0.00008701 1/REarth

Two-line elements (TLE)

Creation date: May 12, 2025, 10:56 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 12, 2025, 6:44 p.m. UTC

TLE line 0: 0 TAURUS R/B

TLE line 1: 1 28255U 04018B 25132.78107068 .00000298 00000-0 87010-4 0 9994

TLE line 2: 2 28255 99.0954 199.1339 0014800 64.3039 295.9680 14.51740554110112

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
COSMOS 2251 DEB LEO 2024-11-03 18:19:59 0.0001642014 509.0 (m) DEBRIS
DMSP 5D-2 F13 DEB SSO 2024-07-06 20:57:35 0.0001469294 335.0 (m) DEBRIS

Associated space launch

ROCSAT 2 (Republic of China Satellite 2) is the second high-resolution Earth observation satellite for the Taiwanese National Space Program Office (NSPO) whose mission is regional remote sensing – to collect data to be used for natural disaster evaluation, agricultural applications, urban planning strategy, environmental monitoring, and ocean surveillance. In addition, the satellite's payload will include an auroral observation instrument.

TAURUS R/B was lifted into orbit during the mission ‘Taurus 3210 | Formosat-2’, on board a Minotaur-C 3210 space rocket.

The launch took place on May 20, 2004, 5:47 p.m. from Space Launch Complex 576E.

For more information about the launch, click the button.

Launch to space Taurus 3210 | Formosat-2
Taurus 3210 | Formosat-2

Agency: N/A

Status: Launch Successful

Launch date: May 20, 2004, 5:47 p.m. UTC

Rocket: Minotaur-C 3210

Launch pad: Space Launch Complex 576E

Location: Vandenberg SFB, CA, USA

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