THEMIS E is a payload in HEO orbit, operated by NASA Goddard Space Flight Center, launched 2007.
Orbital data last updated 3 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | HEO |
| Inclination | 6.5283° |
| Eccentricity | 0.8437049 |
| Period | 1635.6 min |
| Apogee | 78,403 km |
| Perigee | 809 km |
| Mean motion | 0.88041892 rev/day |
| RAAN | 97.0944° |
| Arg of perigee | 218.5457° |
| Mean anomaly | 13.1584° |
| B* | 0.0000e+0 |
| Rev at epoch | 6,606 |
1 30798U 07004E 26184.97903470 -.00000400 00000-0 00000-0 0 99932 30798 6.5283 97.0944 8437049 218.5457 13.1584 0.88041892 66063{
"OBJECT_NAME": "THEMIS E",
"OBJECT_ID": "2007-004E",
"EPOCH": "2026-07-03T23:29:48.598+00:00",
"MEAN_MOTION": 0.88041892,
"ECCENTRICITY": 0.8437049,
"INCLINATION": 6.5283,
"RA_OF_ASC_NODE": 97.0944,
"ARG_OF_PERICENTER": 218.5457,
"MEAN_ANOMALY": 13.1584,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 30798,
"REV_AT_EPOCH": 6606,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.000004,
"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 | THEMIS E |
| Operator | NASA Goddard Space Flight CenterHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | United States |
| Launch date | |
| Launch mass (kg) |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |