EZIE-B is a payload in SSO orbit, operated by JHU-Applied Physics Lab / Jet Propulsion Lab, launched 2025.
| Orbit class | SSO |
| Inclination | 97.6878° |
| Eccentricity | 0.0004709 |
| Period | 96.2 min |
| Apogee | 578 km |
| Perigee | 572 km |
| Mean motion | 14.97371661 rev/day |
| RAAN | 80.0554° |
| Arg of perigee | 112.3399° |
| Mean anomaly | 247.8322° |
| B* | 1.7660e-4 |
| Rev at epoch | 7,165 |
1 63250U 25052AS 26188.15046699 .00001994 00000-0 17660-3 0 99912 63250 97.6878 80.0554 0004709 112.3399 247.8322 14.97371661 71655{
"OBJECT_NAME": "EZIE-B",
"OBJECT_ID": "2025-052AS",
"EPOCH": "2026-07-07T03:36:40.348+00:00",
"MEAN_MOTION": 14.97371661,
"ECCENTRICITY": 0.0004709,
"INCLINATION": 97.6878,
"RA_OF_ASC_NODE": 80.0554,
"ARG_OF_PERICENTER": 112.3399,
"MEAN_ANOMALY": 247.8322,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 63250,
"REV_AT_EPOCH": 7165,
"BSTAR": 0.0001766,
"MEAN_MOTION_DOT": 0.00001994,
"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-B |
| 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 |