ZHUQUE-2E R/B is a rocket body in VLEO orbit, operated by LandSpace Technology, launched 2026.
| Orbit class | VLEO |
| Inclination | 88.9691° |
| Eccentricity | 0.0431844 |
| Period | 94.7 min |
| Apogee | 799 km |
| Perigee | 205 km |
| Mean motion | 15.21362550 rev/day |
| RAAN | 191.6081° |
| Arg of perigee | 224.0079° |
| Mean anomaly | 132.6035° |
| B* | 2.5948e-4 |
| Rev at epoch | 809 |
1 69095U 26105A 26187.56546325 .00112631 -66543-6 25948-3 0 99992 69095 88.9691 191.6081 0431844 224.0079 132.6035 15.21362550 8093{
"OBJECT_NAME": "ZHUQUE-2E R/B",
"OBJECT_ID": "2026-105A",
"EPOCH": "2026-07-06T13:34:16.025+00:00",
"MEAN_MOTION": 15.2136255,
"ECCENTRICITY": 0.04318435,
"INCLINATION": 88.9691,
"RA_OF_ASC_NODE": 191.6081,
"ARG_OF_PERICENTER": 224.0079,
"MEAN_ANOMALY": 132.6035,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 69095,
"REV_AT_EPOCH": 809,
"BSTAR": 0.00025947653,
"MEAN_MOTION_DOT": 0.00112631,
"MEAN_MOTION_DDOT": -6.65425e-7
}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 | ZHUQUE-2E R/B |
| 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 |