▸Orbital parameters

Orbit class	GEO
Inclination	0.0684°
Eccentricity	0.0005808
Period	1436.1 min
Apogee	35,810 km
Perigee	35,761 km
Mean motion	1.00274485 rev/day
RAAN	26.0919°
Arg of perigee	83.4746°
Mean anomaly	254.4520°
B*	0.0000e+0
Rev at epoch	4,472

▸Two-line element set (TLE)

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

1 37775U 11041A 26188.16572669 .00000135 00000-0 00000-0 0 9992

2 37775 0.0684 26.0919 0005808 83.4746 254.4520 1.00274485 44729

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ASTRA 1N",
  "OBJECT_ID": "2011-041A",
  "EPOCH": "2026-07-07T03:58:38.786+00:00",
  "MEAN_MOTION": 1.00274485,
  "ECCENTRICITY": 0.0005808,
  "INCLINATION": 0.0684,
  "RA_OF_ASC_NODE": 26.0919,
  "ARG_OF_PERICENTER": 83.4746,
  "MEAN_ANOMALY": 254.452,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 37775,
  "REV_AT_EPOCH": 4472,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 0.00000135,
  "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 1N
Operator	SES Engineering (Luxembourg) / SES S.A.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Luxembourg
Launch date	Aug 6, 2011HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	5330HIGHvia 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/37775

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