TJS-16 is a payload in GEO orbit, operated by Strategic Support Troops, launched 2025.
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 | 1.1359° |
| Eccentricity | 0.0002939 |
| Period | 1436.1 min |
| Apogee | 35,799 km |
| Perigee | 35,774 km |
| Mean motion | 1.00272015 rev/day |
| RAAN | 81.3849° |
| Arg of perigee | 299.1841° |
| Mean anomaly | 312.2806° |
| B* | 0.0000e+0 |
| Rev at epoch | 454 |
1 63397U 25064A 26183.69857794 -.00000095 00000-0 00000-0 0 99952 63397 1.1359 81.3849 0002939 299.1841 312.2806 1.00272015 4542{
"OBJECT_NAME": "TJS-16",
"OBJECT_ID": "2025-064A",
"EPOCH": "2026-07-02T16:45:57.134+00:00",
"MEAN_MOTION": 1.00272015,
"ECCENTRICITY": 0.0002939,
"INCLINATION": 1.1359,
"RA_OF_ASC_NODE": 81.3849,
"ARG_OF_PERICENTER": 299.1841,
"MEAN_ANOMALY": 312.2806,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 63397,
"REV_AT_EPOCH": 454,
"BSTAR": 0,
"MEAN_MOTION_DOT": -9.5e-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 | TJS-16 |
| 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 |