IRIDIUM 33 DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite IRIDIUM 33 DEB at a glance.

Uptime

10098

Days in orbit

Revolutions

≈ 14.6

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.3

Latest

Satellite identification and parameters

Extended collection of information and parameters for IRIDIUM 33 DEB.

Object identification

Identified? True

Debris? True

Object name: IRIDIUM 33 DEB

International designator: 1997-051FU

Object number (NORAD): 34376

Object ID (CCSDS): 34376

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.739 minutes

Inclination: 86.298 deg

SMA: 7076.522 km

Apoapsis: 717.602 km

Periapsis: 679.172 km

RAAN: 104.7266 deg

Eccentricy: 0.0027153

Argument of periapsis: 192.0745 deg

Mean anomaly: 167.9817 deg

Mean motion: 14.5838757 rev/day

Mean motion (dot): 0.00009392 rev/day2

B* drag term: 0.002012 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, 9:26 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 34376U 97051FU 25127.39342287 .00009392 00000-0 20120-2 0 9990

TLE line 2: 2 34376 86.2980 104.7266 0027153 192.0745 167.9817 14.58387570848063

Live tracking on map

Real-time ground track for satellite IRIDIUM 33 DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 33 DEB.

Target Orbit TCA Probability of collision Miss distance Type
SL-16 DEB LEO 2024-11-13 20:45:17 0.0002230114 817.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-10 18:08:58 0.000506014 236.0 (m) DEBRIS
ATLAS AGENA D R/B LEO 2024-10-03 00:30:32 0.0002249027 908.0 (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 33 DEB was lifted into orbit during the mission ‘Proton-K/17S40 | Iridium 27 to 33’, on board a Proton-K/17S40 space rocket.

The launch took place on Sept. 14, 1997, 1:36 a.m. from 81/23 (81L).

For more information about the launch, click the button.

Launch to space Proton-K/17S40 | Iridium 27 to 33
Proton-K/17S40 | Iridium 27 to 33

Agency: N/A

Status: Launch Successful

Launch date: Sept. 14, 1997, 1:36 a.m. UTC

Rocket: Proton-K/17S40

Launch pad: 81/23 (81L)

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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