View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48918U 26145.61368052 +.00000000 +00000-0 +55770-3 0 00009
2 48918 97.6369 342.0666 0002689 69.1927 290.9633 15.90499627 02
| Epoch (UTC): | 25 May 2026 14:43:41 |
| Eccentricity: | 0.0002689 |
| inclination: | 97.6369° |
| perigee height: | 299 km |
| apogee height: | 303 km |
| right ascension of ascending node: | 342.0666° |
| argument of perigee: | 69.1927° |
| revolutions per day: | 15.90499627 |
| mean anomaly at epoch: | 290.9633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|