ASTRA 1L is a payload in GEO orbit, operated by SES S.A., launched 2007.
| Orbit class | GEO |
| Inclination | 1.3701° |
| Eccentricity | 0.0005435 |
| Period | 1436.1 min |
| Apogee | 35,810 km |
| Perigee | 35,764 km |
| Mean motion | 1.00270338 rev/day |
| RAAN | 81.4273° |
| Arg of perigee | 27.2380° |
| Mean anomaly | 219.6037° |
| B* | 0.0000e+0 |
| Rev at epoch | 4,518 |
1 31306U 07016A 26188.18780806 -.00000170 00000-0 00000-0 0 99992 31306 1.3701 81.4273 0005435 27.2380 219.6037 1.00270338 45181{
"OBJECT_NAME": "ASTRA 1L",
"OBJECT_ID": "2007-016A",
"EPOCH": "2026-07-07T04:30:26.616+00:00",
"MEAN_MOTION": 1.00270338,
"ECCENTRICITY": 0.0005435,
"INCLINATION": 1.3701,
"RA_OF_ASC_NODE": 81.4273,
"ARG_OF_PERICENTER": 27.238,
"MEAN_ANOMALY": 219.6037,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 31306,
"REV_AT_EPOCH": 4518,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.0000017,
"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.
| Name | ASTRA 1L |
| Operator | |
| Country | Luxembourg |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Object class |
| Orbital regime |
| Status |