▸Orbital parameters

Orbit class	GEO
Inclination	0.0595°
Eccentricity	0.0001715
Period	1436.4 min
Apogee	35,799 km
Perigee	35,785 km
Mean motion	1.00252500 rev/day
RAAN	334.6096°
Arg of perigee	269.2406°
Mean anomaly	62.5899°
B*	0.0000e+0
Rev at epoch	739

▸Two-line element set (TLE)

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

1 60086U 24115A 26188.00625964 .00000133 00000-0 00000-0 0 9997

2 60086 0.0595 334.6096 0001715 269.2406 62.5899 1.00252500 7398

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASTRA 1P (SES-24)",
  "OBJECT_ID": "2024-115A",
  "EPOCH": "2026-07-07T00:09:00.833+00:00",
  "MEAN_MOTION": 1.002525,
  "ECCENTRICITY": 0.0001715,
  "INCLINATION": 0.0595,
  "RA_OF_ASC_NODE": 334.6096,
  "ARG_OF_PERICENTER": 269.2406,
  "MEAN_ANOMALY": 62.5899,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60086,
  "REV_AT_EPOCH": 739,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000133,
  "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	ASTRA 1P (SES-24)
Operator	SES S.A.HIGHvia GCAT — Jonathan McDowell's General Catalog SES S.A.MEDIUMvia Wikidata
Country	LuxembourgMEDIUMvia Wikidata
Launch date	Jun 20, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5000HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/60086

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