FALCONSAT

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite FALCONSAT at a glance.

Uptime

9452

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 FALCONSAT.

Object identification

Identified? True

Debris? False

Object name: FALCONSAT

International designator: 2000-004D

Object number (NORAD): 26064

Object ID (CCSDS): 26064

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 100.195 minutes

Inclination: 100.1952 deg

SMA: 7145.916 km

Apoapsis: 793.95 km

Periapsis: 741.611 km

RAAN: 236.6271 deg

Eccentricy: 0.00366217

Argument of periapsis: 225.438 deg

Mean anomaly: 134.3809 deg

Mean motion: 14.37195759 rev/day

Mean motion (dot): 0.00000253 rev/day2

B* drag term: 0.00010420856 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 10:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 12, 2025, 6:08 a.m. UTC

TLE line 0: 0 FALCONSAT

TLE line 1: 1 26064U 00004D 25346.25561447 .00000253 00000-0 10421-3 0 9997

TLE line 2: 2 26064 100.1952 236.6271 0036622 225.4380 134.3809 14.37195759355910

Live tracking on map

Real-time ground track for satellite FALCONSAT.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-12-11 22:57:43 0.0002547388 331.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-12-10 13:59:13 0.0007089656 444.0 (m) DEBRIS
NOAA 16 DEB SSO 2025-06-14 13:15:50 0.0002262014 466.0 (m) DEBRIS
CZ-6A DEB SSO 2025-02-23 19:33:22 0.0001319628 762.0 (m) DEBRIS
DMSP 5D-2 F13 DEB SSO 2025-01-13 13:44:24 0.0003746527 751.0 (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.

FALCONSAT 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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