PICOSAT 6

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite PICOSAT 6 at a glance.

Uptime

9292

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 PICOSAT 6.

Object identification

Identified? True

Debris? False

Object name: PICOSAT 6

International designator: 2000-004M

Object number (NORAD): 26094

Object ID (CCSDS): 26094

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.553 minutes

Inclination: 100.1862 deg

SMA: 7115.356 km

Apoapsis: 760.642 km

Periapsis: 713.801 km

RAAN: 127.7603 deg

Eccentricy: 0.0032915

Argument of periapsis: 99.1677 deg

Mean anomaly: 261.3235 deg

Mean motion: 14.46464488 rev/day

Mean motion (dot): 0.00000689 rev/day2

B* drag term: 0.00020732 1/REarth

Two-line elements (TLE)

Creation date: July 5, 2025, 5:45 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 5, 2025, 6:38 a.m. UTC

TLE line 0: 0 PICOSAT 6

TLE line 1: 1 26094U 00004M 25186.27700272 .00000689 00000-0 20732-3 0 9994

TLE line 2: 2 26094 100.1862 127.7603 0032915 99.1677 261.3235 14.46464488335064

Live tracking on map

Real-time ground track for satellite PICOSAT 6.

In-orbit conjunctions

A list of the most updated potential collisions computed for object PICOSAT 6.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-02-28 20:20:51 0.000341705 221.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2025-02-13 08:56:04 0.0001288348 299.0 (m) DEBRIS
METEOR 2-7 DEB LEO 2025-02-08 00:56:57 0.0002257985 261.0 (m) DEBRIS
CZ-4B DEB SSO 2025-01-16 07:19:21 0.0003546389 672.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-12-30 12:00:05 0.0001361276 409.0 (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.

PICOSAT 6 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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