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

10001

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: 100.967 minutes

Inclination: 86.3306 deg

SMA: 7182.561 km

Apoapsis: 899.321 km

Periapsis: 709.53 km

RAAN: 187.9756 deg

Eccentricy: 0.0132119

Argument of periapsis: 23.7685 deg

Mean anomaly: 336.9532 deg

Mean motion: 14.26211122 rev/day

Mean motion (dot): 0.00006407 rev/day2

B* drag term: 0.0024321 1/REarth

Two-line elements (TLE)

Creation date: May 8, 2025, 3:01 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 3:08 p.m. UTC

TLE line 0: 0 IRIDIUM 47 DEB

TLE line 1: 1 40251U 97082L 25127.63112541 .00006407 00000-0 24321-2 0 9999

TLE line 2: 2 40251 86.3306 187.9756 0132119 23.7685 336.9532 14.26211122543781

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 2025-01-14 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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