IRIDIUM 33 DEB

Satellite information

Favourite Embed

Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite IRIDIUM 33 DEB at a glance.

Uptime

10101

Days in orbit

Revolutions

≈ 14.5

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: 1997-051QA

Object number (NORAD): 35480

Object ID (CCSDS): 35480

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.407 minutes

Inclination: 86.3527 deg

SMA: 7108.375 km

Apoapsis: 741.683 km

Periapsis: 718.796 km

RAAN: 118.6131 deg

Eccentricy: 0.0016099

Argument of periapsis: 104.7924 deg

Mean anomaly: 255.5065 deg

Mean motion: 14.48596056 rev/day

Mean motion (dot): 0.00003242 rev/day2

B* drag term: 0.00085594 1/REarth

Two-line elements (TLE)

Creation date: May 10, 2025, 5:27 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 10, 2025, 9:20 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 35480U 97051QA 25130.38923804 .00003242 00000-0 85594-3 0 9995

TLE line 2: 2 35480 86.3527 118.6131 0016099 104.7924 255.5065 14.48596056838988

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 LEO 2025-02-10 05:56:07 0.000119883 580.0 (m) DEBRIS
CZ-6A DEB LEO 2024-10-31 06:54:23 0.0001303955 393.0 (m) DEBRIS
FALCONSAT SSO 2024-08-17 22:58:47 0.0003016481 215.0 (m) PAYLOAD
COSMOS 2251 DEB LEO 2024-08-16 12:33:30 0.0001159037 250.0 (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

...

Latest news about this satellite

There are no fresh news available about this satellite. Check back as we update our databases every day.


Newsletter sign-up

Weekly statistics, charts and insights to help you stay on top of the space industry.