GEESAT-5 08 is a payload in LEO orbit, operated by GeeSpace, launched 2025.
| Orbit class | LEO |
| Inclination | 49.9780° |
| Eccentricity | 0.0014655 |
| Period | 97.4 min |
| Apogee | 647 km |
| Perigee | 626 km |
| Mean motion | 14.77805908 rev/day |
| RAAN | 306.6266° |
| Arg of perigee | 305.7459° |
| Mean anomaly | 54.2113° |
| B* | 2.0141e-4 |
| Rev at epoch | 4,471 |
1 65557U 25201H 26187.51062368 .00001246 00000-0 20141-3 0 99972 65557 49.9780 306.6266 0014655 305.7459 54.2113 14.77805908 44711{
"OBJECT_NAME": "GEESAT-5 08",
"OBJECT_ID": "2025-201H",
"EPOCH": "2026-07-06T12:15:17.886+00:00",
"MEAN_MOTION": 14.77805908,
"ECCENTRICITY": 0.0014655,
"INCLINATION": 49.978,
"RA_OF_ASC_NODE": 306.6266,
"ARG_OF_PERICENTER": 305.7459,
"MEAN_ANOMALY": 54.2113,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 65557,
"REV_AT_EPOCH": 4471,
"BSTAR": 0.00020141,
"MEAN_MOTION_DOT": 0.00001246,
"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-5 08 |
| 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 |