View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15378U 26064.68310406 +.00000000 +00000-0 +49480-4 0 00002
2 15378 64.9941 329.2665 0039141 3.3123 356.8188 13.83706089 06
| Epoch (UTC): | 05 March 2026 16:23:40 |
| Eccentricity: | 0.0039141 |
| inclination: | 64.9941° |
| perigee height: | 922 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 329.2665° |
| argument of perigee: | 3.3123° |
| revolutions per day: | 13.83706089 |
| mean anomaly at epoch: | 356.8188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|