OPAL

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite OPAL 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 OPAL.

Object identification

Identified? True

Debris? False

Object name: OPAL

International designator: 2000-004C

Object number (NORAD): 26063

Object ID (CCSDS): 26063

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 100.156 minutes

Inclination: 100.2192 deg

SMA: 7144.038 km

Apoapsis: 792.039 km

Periapsis: 739.768 km

RAAN: 341.7768 deg

Eccentricy: 0.0036584

Argument of periapsis: 107.2579 deg

Mean anomaly: 253.2611 deg

Mean motion: 14.37762327 rev/day

Mean motion (dot): 0.00000216 rev/day2

B* drag term: 0.000090669 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, 8:03 a.m. UTC

TLE line 0: 0 OPAL

TLE line 1: 1 26063U 00004C 25125.33551191 .00000216 00000-0 90669-4 0 9997

TLE line 2: 2 26063 100.2192 341.7768 0036584 107.2579 253.2611 14.37762327324671

Live tracking on map

Real-time ground track for satellite OPAL.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 2251 DEB LEO 2025-04-06 19:37:59 0.0001209291 333.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-31 13:03:22 0.0001842184 722.0 (m) DEBRIS
CZ-6A DEB LEO 2024-11-24 07:33:22 0.0007166333 426.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2024-10-11 22:54:59 0.0007513447 121.0 (m) DEBRIS
DMSP 5D-2 F15 DEB SSO 2024-09-26 02:14:48 0.0002185693 309.0 (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.

OPAL 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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