TJS-10 is a payload in GEO orbit, operated by Strategic Support Troops, launched 2023.
Orbital data last updated 4 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | GEO |
| Inclination | 2.5821° |
| Eccentricity | 0.0004215 |
| Period | 1436.1 min |
| Apogee | 35,805 km |
| Perigee | 35,769 km |
| Mean motion | 1.00269643 rev/day |
| RAAN | 80.3140° |
| Arg of perigee | 104.6482° |
| Mean anomaly | 98.4495° |
| B* | 0.0000e+0 |
| Rev at epoch | 969 |
1 58204U 23169A 26183.75054779 -.00000239 00000-0 00000-0 0 99992 58204 2.5821 80.3140 0004215 104.6482 98.4495 1.00269643 9696{
"OBJECT_NAME": "TJS-10",
"OBJECT_ID": "2023-169A",
"EPOCH": "2026-07-02T18:00:47.329+00:00",
"MEAN_MOTION": 1.00269643,
"ECCENTRICITY": 0.0004215,
"INCLINATION": 2.5821,
"RA_OF_ASC_NODE": 80.314,
"ARG_OF_PERICENTER": 104.6482,
"MEAN_ANOMALY": 98.4495,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 58204,
"REV_AT_EPOCH": 969,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.00000239,
"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 | TJS-10 |
| 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 |