EZIE-C is a payload in SSO orbit, operated by JHU-Applied Physics Lab / Jet Propulsion Lab, launched 2025.
| Orbit class | SSO |
| Inclination | 97.6846° |
| Eccentricity | 0.0003795 |
| Period | 96.2 min |
| Apogee | 577 km |
| Perigee | 572 km |
| Mean motion | 14.97441318 rev/day |
| RAAN | 79.8853° |
| Arg of perigee | 129.3827° |
| Mean anomaly | 230.7732° |
| B* | 2.2768e-4 |
| Rev at epoch | 7,165 |
1 63249U 25052AR 26188.15521067 .00002592 00000-0 22768-3 0 99962 63249 97.6846 79.8853 0003795 129.3827 230.7732 14.97441318 71657{
"OBJECT_NAME": "EZIE-C",
"OBJECT_ID": "2025-052AR",
"EPOCH": "2026-07-07T03:43:30.202+00:00",
"MEAN_MOTION": 14.97441318,
"ECCENTRICITY": 0.0003795,
"INCLINATION": 97.6846,
"RA_OF_ASC_NODE": 79.8853,
"ARG_OF_PERICENTER": 129.3827,
"MEAN_ANOMALY": 230.7732,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 63249,
"REV_AT_EPOCH": 7165,
"BSTAR": 0.00022768,
"MEAN_MOTION_DOT": 0.00002592,
"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 | EZIE-C |
| Operator | JHU-Applied Physics Lab / Jet Propulsion LabHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 10 |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |