TIANQI-39 is a payload in LEO orbit, operated by Guodian HiTech Technology Co Ltd., launched 2026.
Orbital data last updated 7 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | LEO |
| Inclination | 44.9816° |
| Eccentricity | 0.0013885 |
| Period | 102.8 min |
| Apogee | 901 km |
| Perigee | 881 km |
| Mean motion | 14.00833067 rev/day |
| RAAN | 22.6279° |
| Arg of perigee | 45.6434° |
| Mean anomaly | 314.5534° |
| B* | 1.0159e-4 |
| Rev at epoch | 2,318 |
1 67478U 26010C 26180.57179163 .00000023 00000-0 10159-3 0 99912 67478 44.9816 22.6279 0013885 45.6434 314.5534 14.00833067 23186{
"OBJECT_NAME": "TIANQI-39",
"OBJECT_ID": "2026-010C",
"EPOCH": "2026-06-29T13:43:22.797+00:00",
"MEAN_MOTION": 14.00833067,
"ECCENTRICITY": 0.00138852,
"INCLINATION": 44.9816,
"RA_OF_ASC_NODE": 22.6279,
"ARG_OF_PERICENTER": 45.6434,
"MEAN_ANOMALY": 314.5534,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 67478,
"REV_AT_EPOCH": 2318,
"BSTAR": 0.00010159373,
"MEAN_MOTION_DOT": 2.3e-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 | TIANQI-39 |
| 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 |