STEX

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite STEX at a glance.

Uptime

9774

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

LEO

Low Earth Orbit

Inclination

85.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for STEX.

Object identification

Identified? True

Debris? False

Object name: STEX

International designator: 1998-055A

Object number (NORAD): 25489

Object ID (CCSDS): 25489

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 99.217 minutes

Inclination: 84.9836 deg

SMA: 7099.335 km

Apoapsis: 728.975 km

Periapsis: 713.426 km

RAAN: 181.85 deg

Eccentricy: 0.0010951

Argument of periapsis: 115.9293 deg

Mean anomaly: 244.304 deg

Mean motion: 14.51363628 rev/day

Mean motion (dot): 0.00000462 rev/day2

B* drag term: 0.00011056 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, 11:41 a.m. UTC

TLE line 0: 0 STEX

TLE line 1: 1 25489U 98055A 25187.48699186 .00000462 00000-0 11056-3 0 9997

TLE line 2: 2 25489 84.9836 181.8500 0010951 115.9293 244.3040 14.51363628413180

Live tracking on map

Real-time ground track for satellite STEX.

In-orbit conjunctions

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

Target Orbit TCA Probability of collision Miss distance Type
NOAA 16 DEB SSO 2025-06-20 12:16:34 0.000668123 746.0 (m) DEBRIS
CZ-4 DEB SSO 2025-06-14 14:35:09 0.0003023308 440.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-03-30 15:17:17 0.0003653638 268.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-12 09:36:40 0.0001794229 163.0 (m) DEBRIS
THORAD AGENA D DEB LEO 2024-10-16 15:11:04 0.000292892 885.0 (m) DEBRIS

Associated space launch

The STEX (Space Technology Experiments) satellite carried 29 new technologies intended to result in lower cost and higher performance spacecraft for future missions.

STEX was lifted into orbit during the mission ‘Minotaur | NROL-8’, on board a Minotaur space rocket.

The launch took place on Oct. 3, 1998, 10:04 a.m. from Space Launch Complex 576E.

For more information about the launch, click the button.

Launch to space Minotaur | NROL-8
Minotaur | NROL-8

Agency: N/A

Status: Launch Successful

Launch date: Oct. 3, 1998, 10:04 a.m. UTC

Rocket: Minotaur

Launch pad: Space Launch Complex 576E

Location: Vandenberg SFB, CA, USA

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