CHUTIAN-2 A is a payload in SSO orbit, operated by China Aerospace Science and Industry Corp., launched 2025.
Orbital data last updated 3 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | SSO |
| Inclination | 98.2517° |
| Eccentricity | 0.0012323 |
| Period | 99.3 min |
| Apogee | 734 km |
| Perigee | 716 km |
| Mean motion | 14.50220974 rev/day |
| RAAN | 250.5795° |
| Arg of perigee | 283.4185° |
| Mean anomaly | 76.5635° |
| B* | 1.6258e-4 |
| Rev at epoch | 3,429 |
1 66409U 25256A 26184.72749358 .00000589 00000-0 16258-3 0 99982 66409 98.2517 250.5795 0012323 283.4185 76.5635 14.50220974 34298{
"OBJECT_NAME": "CHUTIAN-2 A",
"OBJECT_ID": "2025-256A",
"EPOCH": "2026-07-03T17:27:35.445+00:00",
"MEAN_MOTION": 14.50220974,
"ECCENTRICITY": 0.0012323,
"INCLINATION": 98.2517,
"RA_OF_ASC_NODE": 250.5795,
"ARG_OF_PERICENTER": 283.4185,
"MEAN_ANOMALY": 76.5635,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 66409,
"REV_AT_EPOCH": 3429,
"BSTAR": 0.00016258,
"MEAN_MOTION_DOT": 0.00000589,
"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 | CHUTIAN-2 A |
| 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 |