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

10159

Days in orbit

Revolutions

≈ 14.8

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: 1997-051CN

Object number (NORAD): 34079

Object ID (CCSDS): 34079

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 97.375 minutes

Inclination: 86.3779 deg

SMA: 7011.21 km

Apoapsis: 637.68 km

Periapsis: 628.47 km

RAAN: 80.6754 deg

Eccentricy: 0.0006568

Argument of periapsis: 147.0632 deg

Mean anomaly: 241.2651 deg

Mean motion: 14.78813229 rev/day

Mean motion (dot): 0.00006824 rev/day2

B* drag term: 0.00092435 1/REarth

Two-line elements (TLE)

Creation date: July 7, 2025, 5:18 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 4:34 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 34079U 97051CN 25187.69061487 .00006824 00000-0 92435-3 0 9995

TLE line 2: 2 34079 86.3779 80.6754 0006568 147.0632 241.2651 14.78813229866245

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
CZ-6A DEB SSO 2025-07-05 17:15:39 0.0005592026 54.0 (m) DEBRIS
CZ-6A DEB LEO 2025-01-30 15:33:31 0.0001791621 429.0 (m) DEBRIS
CZ-6A DEB LEO 2025-01-16 05:12:19 0.0001230715 91.0 (m) DEBRIS
SUNSAT SSO 2024-12-22 05:17:56 0.0002830603 257.0 (m) PAYLOAD
CZ-6A DEB SSO 2024-11-14 18:30:09 0.0001057731 454.0 (m) DEBRIS

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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