PICOSAT 5

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite PICOSAT 5 at a glance.

Uptime

9293

Days in orbit

Revolutions

≈ 14.6

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

100.2

Latest

Satellite identification and parameters

Extended collection of information and parameters for PICOSAT 5.

Object identification

Identified? True

Debris? False

Object name: PICOSAT 5

International designator: 2000-004L

Object number (NORAD): 26093

Object ID (CCSDS): 26093

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.454 minutes

Inclination: 100.1869 deg

SMA: 7062.887 km

Apoapsis: 702.626 km

Periapsis: 666.878 km

RAAN: 249.1124 deg

Eccentricy: 0.0025307

Argument of periapsis: 155.603 deg

Mean anomaly: 204.6368 deg

Mean motion: 14.62612738 rev/day

Mean motion (dot): 0.00002119 rev/day2

B* drag term: 0.00042862 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 6:05 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 9:18 a.m. UTC

TLE line 0: 0 PICOSAT 5

TLE line 1: 1 26093U 00004L 25187.38789232 .00002119 00000-0 42862-3 0 9997

TLE line 2: 2 26093 100.1869 249.1124 0025307 155.6030 204.6368 14.62612738341857

Live tracking on map

Real-time ground track for satellite PICOSAT 5.

In-orbit conjunctions

A list of the most updated potential collisions computed for object PICOSAT 5.

Target Orbit TCA Probability of collision Miss distance Type
SL-8 R/B SSO 2025-01-30 09:07:09 0.0005482334 573.0 (m) ROCKET BODY
CZ-4 DEB SSO 2025-01-06 08:14:34 0.00010682 326.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2024-11-12 16:39:55 0.0001946449 593.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-08-22 11:16:21 0.0001593239 482.0 (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 5 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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