View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53398U 26145.38526817 +.00000000 +00000-0 +26956-3 0 00000
2 53398 53.2133 139.8220 0001576 65.9716 294.1441 15.08826977 03
| Epoch (UTC): | 25 May 2026 09:14:47 |
| Eccentricity: | 0.0001576 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 139.8220° |
| argument of perigee: | 65.9716° |
| revolutions per day: | 15.08826977 |
| mean anomaly at epoch: | 294.1441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|