XINGCHI-1 02A is a payload in SSO orbit, operated by Elliptic SpaceTime (Beijing) Tech Co Ltd., launched 2023.
| Orbit class | SSO |
| Inclination | 97.9261° |
| Eccentricity | 0.0012916 |
| Period | 97.0 min |
| Apogee | 625 km |
| Perigee | 607 km |
| Mean motion | 14.84329437 rev/day |
| RAAN | 270.9525° |
| Arg of perigee | 81.5287° |
| Mean anomaly | 278.7390° |
| B* | 1.6099e-4 |
| Rev at epoch | 14,009 |
1 58496U 23187A 26188.22702242 .00001298 00000-0 16099-3 0 99972 58496 97.9261 270.9525 0012916 81.5287 278.7390 14.84329437140093{
"OBJECT_NAME": "XINGCHI-1 02A",
"OBJECT_ID": "2023-187A",
"EPOCH": "2026-07-07T05:26:54.737+00:00",
"MEAN_MOTION": 14.84329437,
"ECCENTRICITY": 0.0012916,
"INCLINATION": 97.9261,
"RA_OF_ASC_NODE": 270.9525,
"ARG_OF_PERICENTER": 81.5287,
"MEAN_ANOMALY": 278.739,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 58496,
"REV_AT_EPOCH": 14009,
"BSTAR": 0.00016099,
"MEAN_MOTION_DOT": 0.00001298,
"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 | XINGCHI-1 02A |
| 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 |