IRIDIUM 47 DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite IRIDIUM 47 DEB at a glance.

Uptime

10221

Days in orbit

Revolutions

≈ 14.3

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.3

Latest

Satellite identification and parameters

Extended collection of information and parameters for IRIDIUM 47 DEB.

Object identification

Identified? True

Debris? True

Object name: IRIDIUM 47 DEB

International designator: 1997-082L

Object number (NORAD): 40251

Object ID (CCSDS): 40251

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 100.678 minutes

Inclination: 86.3216 deg

SMA: 7168.852 km

Apoapsis: 878.346 km

Periapsis: 703.088 km

RAAN: 95.8408 deg

Eccentricy: 0.01222359

Argument of periapsis: 35.6477 deg

Mean anomaly: 325.2801 deg

Mean motion: 14.30304057 rev/day

Mean motion (dot): 0.00012168 rev/day2

B* drag term: 0.0043127595 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, 6:55 a.m. UTC

TLE line 0: 0 IRIDIUM 47 DEB

TLE line 1: 1 40251U 97082L 25346.28835274 .00012168 00000-0 43128-2 0 9995

TLE line 2: 2 40251 86.3216 95.8408 0122236 35.6477 325.2801 14.30304057574983

Live tracking on map

Real-time ground track for satellite IRIDIUM 47 DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 47 DEB.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2025-11-23 20:45:51 0.0001034614 129.0 (m) DEBRIS
COSMOS 540 LEO 2025-08-13 15:13:51 0.0002841589 608.0 (m) PAYLOAD
FENGYUN 1C DEB SSO 2025-05-09 07:27:09 0.0002965871 18.0 (m) DEBRIS
CZ-6A DEB LEO 2025-01-14 10:00:35 0.0001993152 669.0 (m) DEBRIS
SL-14 R/B LEO 2024-08-20 10:35:53 0.0003561715 212.0 (m) ROCKET BODY

Associated space launch

Iridium provides global mobile telecommunications services using a constellation of 66 low earth orbit satellites in a 86.4° inclined orbit. Although 77 satellites were originally envisioned for the system and spawned the name based on the 77th element in the periodic table, the system has been scaled back. Motorola's Satellite Communications Group designed and manufactured the Iridium satellites with Lockheed Martin providing the LM-700A spacecraft buses.

IRIDIUM 47 DEB was lifted into orbit during the mission ‘Delta II | Iridium 45 to 49’, on board a Delta II space rocket.

The launch took place on Dec. 20, 1997, 1:16 p.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Delta II | Iridium 45 to 49
Delta II | Iridium 45 to 49

Agency: N/A

Status: Launch Successful

Launch date: Dec. 20, 1997, 1:16 p.m. UTC

Rocket: Delta II

Launch pad: Space Launch Complex 2W

Location: Vandenberg SFB, CA, USA

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