▸Orbital parameters

Orbit class	LEO
Inclination	86.3953°
Eccentricity	0.0002197
Period	100.4 min
Apogee	779 km
Perigee	776 km
Mean motion	14.34218694 rev/day
RAAN	80.1301°
Arg of perigee	77.3658°
Mean anomaly	282.7783°
B*	5.9226e-5
Rev at epoch	49,613

▸Two-line element set (TLE)

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

1 41922U 17003F 26188.16344860 .00000186 00000-0 59226-4 0 9999

2 41922 86.3953 80.1301 0002197 77.3658 282.7783 14.34218694496134

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IRIDIUM 104",
  "OBJECT_ID": "2017-003F",
  "EPOCH": "2026-07-07T03:55:21.959+00:00",
  "MEAN_MOTION": 14.34218694,
  "ECCENTRICITY": 0.0002197,
  "INCLINATION": 86.3953,
  "RA_OF_ASC_NODE": 80.1301,
  "ARG_OF_PERICENTER": 77.3658,
  "MEAN_ANOMALY": 282.7783,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 41922,
  "REV_AT_EPOCH": 49613,
  "BSTAR": 0.000059226,
  "MEAN_MOTION_DOT": 0.00000186,
  "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 104
Operator	Iridium Satellite LLCHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jan 14, 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/41922

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