MINOTAUR DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite MINOTAUR DEB at a glance.

Uptime

9231

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

100.2

Latest

Satellite identification and parameters

Extended collection of information and parameters for MINOTAUR DEB.

Object identification

Identified? True

Debris? True

Object name: MINOTAUR DEB

International designator: 2000-004G

Object number (NORAD): 26079

Object ID (CCSDS): 26079

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.411 minutes

Inclination: 100.2038 deg

SMA: 7108.605 km

Apoapsis: 751.964 km

Periapsis: 708.976 km

RAAN: 79.3153 deg

Eccentricy: 0.0030237

Argument of periapsis: 239.9677 deg

Mean anomaly: 148.3302 deg

Mean motion: 14.48525592 rev/day

Mean motion (dot): 0.00001589 rev/day2

B* drag term: 0.00043743 1/REarth

Two-line elements (TLE)

Creation date: May 6, 2025, 3:54 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 5, 2025, 8:27 p.m. UTC

TLE line 0: 0 MINOTAUR DEB

TLE line 1: 1 26079U 00004G 25125.85231492 .00001589 00000-0 43743-3 0 9994

TLE line 2: 2 26079 100.2038 79.3153 0030237 239.9677 148.3302 14.48525592328612

Live tracking on map

Real-time ground track for satellite MINOTAUR DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object MINOTAUR DEB.

Target Orbit TCA Probability of collision Miss distance Type
SL-8 R/B LEO 2025-05-01 22:18:47 0.0001486052 617.0 (m) ROCKET BODY
CZ-6A DEB LEO 2025-01-27 15:57:21 0.0001149291 107.0 (m) DEBRIS
CZ-6A DEB LEO 2024-11-14 06:07:12 0.0008579661 265.0 (m) DEBRIS
CZ-6A DEB SSO 2024-11-11 22:29:31 0.0006122738 427.0 (m) DEBRIS
CZ-6A DEB SSO 2024-09-25 11:59:56 0.0002446121 333.0 (m) DEBRIS

Associated space launch

The JAWSAT (Joint Air Force Academy / Weber State University Satellite) project was developed by students working alongside aerospace professionals. Initially designed with a pulsed-plasma thruster to train Air Force Academy cadets (see JAWSAT), the mission has since evolved to include the efforts of several universities, local aerospace companies, the Air Force Academy, the Air Force Research Laboratory, and NASA. Utilizing breakthrough technologies, JAWSAT deployed four satellites when it reached orbit. The onboard imaging system recorded the deployment of each payload with its six digital cameras. The first free-flying Academy satellite, FalconSat-1 carried the CHAWS (Charging Hazards and Wake Studies) experiment developed by the Physics Department at the Academy.

MINOTAUR DEB was lifted into orbit during the mission ‘Minotaur I | JAWSAT & FalconSat 1’, on board a Minotaur I space rocket.

The launch took place on Jan. 27, 2000, 3:03 a.m. from Space Launch Complex 8.

For more information about the launch, click the button.

Launch to space Minotaur I | JAWSAT & FalconSat 1
Minotaur I | JAWSAT & FalconSat 1

Agency: N/A

Status: Launch Successful

Launch date: Jan. 27, 2000, 3:03 a.m. UTC

Rocket: Minotaur I

Launch pad: Space Launch Complex 8

Location: Vandenberg SFB, CA, USA

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