ASTRA 1KR is a payload in GEO orbit, operated by SES Astra, launched 2006.
| Orbit class | GEO |
| Inclination | 0.5221° |
| Eccentricity | 0.0003428 |
| Period | 1436.1 min |
| Apogee | 35,801 km |
| Perigee | 35,772 km |
| Mean motion | 1.00272824 rev/day |
| RAAN | 83.2153° |
| Arg of perigee | 18.8059° |
| Mean anomaly | 261.7744° |
| B* | 0.0000e+0 |
| Rev at epoch | 4,589 |
1 29055U 06012A 26188.16572669 .00000134 00000-0 00000-0 0 99952 29055 0.5221 83.2153 0003428 18.8059 261.7744 1.00272824 45896{
"OBJECT_NAME": "ASTRA 1KR",
"OBJECT_ID": "2006-012A",
"EPOCH": "2026-07-07T03:58:38.786+00:00",
"MEAN_MOTION": 1.00272824,
"ECCENTRICITY": 0.0003428,
"INCLINATION": 0.5221,
"RA_OF_ASC_NODE": 83.2153,
"ARG_OF_PERICENTER": 18.8059,
"MEAN_ANOMALY": 261.7744,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 29055,
"REV_AT_EPOCH": 4589,
"BSTAR": 0,
"MEAN_MOTION_DOT": 0.00000134,
"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 1KR |
| Operator | |
| Country | Luxembourg |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |