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

10099

Days in orbit

Revolutions

≈ 14.1

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.4

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: 1997-051JZ

Object number (NORAD): 34648

Object ID (CCSDS): 34648

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 102.251 minutes

Inclination: 86.3972 deg

SMA: 7243.356 km

Apoapsis: 1001.711 km

Periapsis: 728.73 km

RAAN: 10.6409 deg

Eccentricy: 0.0188435

Argument of periapsis: 269.7688 deg

Mean anomaly: 88.1901 deg

Mean motion: 14.08293088 rev/day

Mean motion (dot): 0.00002726 rev/day2

B* drag term: 0.0013478 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, 10:20 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 34648U 97051JZ 25125.93123287 .00002726 00000-0 13478-2 0 9999

TLE line 2: 2 34648 86.3972 10.6409 0188435 269.7688 88.1901 14.08293088818510

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
COSMOS 1670 LEO 2025-04-10 19:21:01 0.000354225 584.0 (m) PAYLOAD
SL-8 R/B LEO 2025-03-11 11:07:20 0.000149247 277.0 (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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