GJZ 02 is a payload in LEO orbit, operated by China Aerospace Corp, launched 2024.
| Orbit class | LEO |
| Inclination | 59.9154° |
| Eccentricity | 0.0006665 |
| Period | 104.7 min |
| Apogee | 986 km |
| Perigee | 976 km |
| Mean motion | 13.75207607 rev/day |
| RAAN | 190.2298° |
| Arg of perigee | 89.9429° |
| Mean anomaly | 270.2342° |
| B* | 3.5516e-5 |
| Rev at epoch | 7,903 |
1 62291U 24238B 26188.19358166 -.00000085 00000-0 35516-4 0 99912 62291 59.9154 190.2298 0006665 89.9429 270.2342 13.75207607 79037{
"OBJECT_NAME": "GJZ 02",
"OBJECT_ID": "2024-238B",
"EPOCH": "2026-07-07T04:38:45.455+00:00",
"MEAN_MOTION": 13.75207607,
"ECCENTRICITY": 0.0006665,
"INCLINATION": 59.9154,
"RA_OF_ASC_NODE": 190.2298,
"ARG_OF_PERICENTER": 89.9429,
"MEAN_ANOMALY": 270.2342,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 62291,
"REV_AT_EPOCH": 7903,
"BSTAR": 0.000035516,
"MEAN_MOTION_DOT": -8.5e-7,
"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 | GJZ 02 |
| 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 |