GEESAT-1 05 is a payload in LEO orbit, operated by GeeSpace, launched 2022.
| Orbit class | LEO |
| Inclination | 49.9865° |
| Eccentricity | 0.0002231 |
| Period | 95.9 min |
| Apogee | 566 km |
| Perigee | 563 km |
| Mean motion | 15.00828145 rev/day |
| RAAN | 85.7669° |
| Arg of perigee | 123.2597° |
| Mean anomaly | 236.8563° |
| B* | 2.8306e-4 |
| Rev at epoch | 22,320 |
1 52789U 22058E 26188.12440536 .00003378 00000-0 28306-3 0 99912 52789 49.9865 85.7669 0002231 123.2597 236.8563 15.00828145223208{
"OBJECT_NAME": "GEESAT-1 05",
"OBJECT_ID": "2022-058E",
"EPOCH": "2026-07-07T02:59:08.623+00:00",
"MEAN_MOTION": 15.00828145,
"ECCENTRICITY": 0.0002231,
"INCLINATION": 49.9865,
"RA_OF_ASC_NODE": 85.7669,
"ARG_OF_PERICENTER": 123.2597,
"MEAN_ANOMALY": 236.8563,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 52789,
"REV_AT_EPOCH": 22320,
"BSTAR": 0.00028306,
"MEAN_MOTION_DOT": 0.00003378,
"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 | GEESAT-1 05 |
| Operator | |
| Country | China |
| 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 |