TJS-4 is a payload in GEO orbit, operated by China Aerospace Corp, launched 2019.
| Orbit class | GEO |
| Inclination | 0.0629° |
| Eccentricity | 0.0003566 |
| Period | 1436.1 min |
| Apogee | 35,802 km |
| Perigee | 35,772 km |
| Mean motion | 1.00270811 rev/day |
| RAAN | 87.3169° |
| Arg of perigee | 320.9915° |
| Mean anomaly | 18.5589° |
| B* | 0.0000e+0 |
| Rev at epoch | 2,473 |
1 44637U 19070A 26188.16161463 -.00000155 00000-0 00000-0 0 99962 44637 0.0629 87.3169 0003566 320.9915 18.5589 1.00270811 24738{
"OBJECT_NAME": "TJS-4",
"OBJECT_ID": "2019-070A",
"EPOCH": "2026-07-07T03:52:43.504+00:00",
"MEAN_MOTION": 1.00270811,
"ECCENTRICITY": 0.0003566,
"INCLINATION": 0.0629,
"RA_OF_ASC_NODE": 87.3169,
"ARG_OF_PERICENTER": 320.9915,
"MEAN_ANOMALY": 18.5589,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 44637,
"REV_AT_EPOCH": 2473,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.00000155,
"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-4 |
| 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 |