▸Orbital parameters

Orbit class	GEO
Inclination	0.0130°
Eccentricity	0.0000405
Period	1436.0 min
Apogee	35,787 km
Perigee	35,784 km
Mean motion	1.00275567 rev/day
RAAN	52.9192°
Arg of perigee	98.8720°
Mean anomaly	100.5402°
B*	0.0000e+0
Rev at epoch	5,015

▸Two-line element set (TLE)

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

1 38867U 12057A 26188.05637558 -.00000270 00000-0 00000-0 0 9991

2 38867 0.0130 52.9192 0000405 98.8720 100.5402 1.00275567 50155

▸ source OMM (JSON)

{
  "OBJECT_NAME": "INTELSAT 23 (IS-23)",
  "OBJECT_ID": "2012-057A",
  "EPOCH": "2026-07-07T01:21:10.85+00:00",
  "MEAN_MOTION": 1.00275567,
  "ECCENTRICITY": 0.0000405,
  "INCLINATION": 0.013,
  "RA_OF_ASC_NODE": 52.9192,
  "ARG_OF_PERICENTER": 98.872,
  "MEAN_ANOMALY": 100.5402,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 38867,
  "REV_AT_EPOCH": 5015,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -0.0000027,
  "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	INTELSAT 23 (IS-23)
Operator	Intelsat S.A., US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree IntelsatMEDIUMvia Wikidata
Country	United States
Launch date	Oct 14, 2012HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	3200HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/38867

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