▸Orbital parameters

Orbit class	LEO
Inclination	86.3981°
Eccentricity	0.0002052
Period	100.4 min
Apogee	779 km
Perigee	776 km
Mean motion	14.34217455 rev/day
RAAN	313.8389°
Arg of perigee	95.4828°
Mean anomaly	264.6602°
B*	-2.0486e-5
Rev at epoch	44,692

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 43075U 17083F 26187.87068372 -.00000038 00000-0 -20486-4 0 9990

2 43075 86.3981 313.8389 0002052 95.4828 264.6602 14.34217455446923

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRIDIUM 134",
  "OBJECT_ID": "2017-083F",
  "EPOCH": "2026-07-06T20:53:47.073+00:00",
  "MEAN_MOTION": 14.34217455,
  "ECCENTRICITY": 0.0002052,
  "INCLINATION": 86.3981,
  "RA_OF_ASC_NODE": 313.8389,
  "ARG_OF_PERICENTER": 95.4828,
  "MEAN_ANOMALY": 264.6602,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 43075,
  "REV_AT_EPOCH": 44692,
  "BSTAR": -0.000020486,
  "MEAN_MOTION_DOT": -3.8e-7,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	IRIDIUM 134
Operator	Iridium Satellite LLCHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Dec 23, 2017HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	860HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/43075

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.