ASUSAT

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite ASUSAT at a glance.

Uptime

9232

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

100.2

Latest

Satellite identification and parameters

Extended collection of information and parameters for ASUSAT.

Object identification

Identified? True

Debris? False

Object name: ASUSAT

International designator: 2000-004E

Object number (NORAD): 26065

Object ID (CCSDS): 26065

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 100.138 minutes

Inclination: 100.2187 deg

SMA: 7143.214 km

Apoapsis: 791.36 km

Periapsis: 738.799 km

RAAN: 345.9133 deg

Eccentricy: 0.0036791

Argument of periapsis: 104.5453 deg

Mean anomaly: 255.9813 deg

Mean motion: 14.38011084 rev/day

Mean motion (dot): 0.00000241 rev/day2

B* drag term: 0.00009853 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, 9:02 p.m. UTC

TLE line 0: 0 ASUSAT

TLE line 1: 1 26065U 00004E 25125.87674456 .00000241 00000-0 98530-4 0 9991

TLE line 2: 2 26065 100.2187 345.9133 0036791 104.5453 255.9813 14.38011084325010

Live tracking on map

Real-time ground track for satellite ASUSAT.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 2251 DEB LEO 2025-01-25 01:48:48 0.000298617 642.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-30 22:34:22 0.0001115617 704.0 (m) DEBRIS
COSMOS 1275 DEB LEO 2024-12-29 10:50:04 0.0001417343 775.0 (m) DEBRIS
DMSP 5D-2 F13 DEB SSO 2024-11-14 15:30:43 0.0002072104 312.0 (m) DEBRIS
CZ-6A DEB LEO 2024-11-05 09:21:02 0.0002250333 659.0 (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.

ASUSAT 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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