TJS-3 is a payload in GEO orbit, operated by China Aerospace Corp, launched 2018.
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 | 2.5826° |
| Eccentricity | 0.0002326 |
| Period | 1436.0 min |
| Apogee | 35,795 km |
| Perigee | 35,776 km |
| Mean motion | 1.00275771 rev/day |
| RAAN | 80.3162° |
| Arg of perigee | 74.4390° |
| Mean anomaly | 191.5459° |
| B* | 0.0000e+0 |
| Rev at epoch | 2,757 |
1 43874U 18110A 26183.77045742 -.00000207 00000-0 00000-0 0 99932 43874 2.5826 80.3162 0002326 74.4390 191.5459 1.00275771 27576{
"OBJECT_NAME": "TJS-3",
"OBJECT_ID": "2018-110A",
"EPOCH": "2026-07-02T18:29:27.521+00:00",
"MEAN_MOTION": 1.00275771,
"ECCENTRICITY": 0.0002326,
"INCLINATION": 2.5826,
"RA_OF_ASC_NODE": 80.3162,
"ARG_OF_PERICENTER": 74.439,
"MEAN_ANOMALY": 191.5459,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 43874,
"REV_AT_EPOCH": 2757,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.00000207,
"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-3 |
| 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 |