▸Orbital parameters

Orbit class	GEO
Inclination	0.0199°
Eccentricity	0.0001997
Period	1436.1 min
Apogee	35,796 km
Perigee	35,779 km
Mean motion	1.00270215 rev/day
RAAN	67.0885°
Arg of perigee	23.9896°
Mean anomaly	58.5838°
B*	0.0000e+0
Rev at epoch	1,373

▸Two-line element set (TLE)

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

1 53960U 22123A 26187.91080358 -.00000086 00000-0 00000-0 0 9996

2 53960 0.0199 67.0885 0001997 23.9896 58.5838 1.00270215 13730

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SES-20",
  "OBJECT_ID": "2022-123A",
  "EPOCH": "2026-07-06T21:51:33.429+00:00",
  "MEAN_MOTION": 1.00270215,
  "ECCENTRICITY": 0.0001997,
  "INCLINATION": 0.0199,
  "RA_OF_ASC_NODE": 67.0885,
  "ARG_OF_PERICENTER": 23.9896,
  "MEAN_ANOMALY": 58.5838,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 53960,
  "REV_AT_EPOCH": 1373,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": -8.6e-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	SES-20
Operator	SES S.A. (Princeton)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Oct 4, 2022HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1499HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree 1500MEDIUMvia Wikidata

▸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/53960

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