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

7719

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: 99.189 minutes

Inclination: 99.0936 deg

SMA: 7097.994 km

Apoapsis: 728.992 km

Periapsis: 710.726 km

RAAN: 259.7546 deg

Eccentricy: 0.0012867

Argument of periapsis: 252.3732 deg

Mean anomaly: 107.6056 deg

Mean motion: 14.51775153 rev/day

Mean motion (dot): 0.00000158 rev/day2

B* drag term: 0.000052177 1/REarth

Two-line elements (TLE)

Creation date: July 7, 2025, 10:56 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 7, 2025, 7:32 p.m. UTC

TLE line 0: 0 TAURUS R/B

TLE line 1: 1 28255U 04018B 25188.81416385 .00000158 00000-0 52177-4 0 9995

TLE line 2: 2 28255 99.0936 259.7546 0012867 252.3732 107.6056 14.51775153118246

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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