View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57493U 26145.51919816 +.00000000 +00000-0 +00000-0 0 00009
2 57493 0.0178 328.1582 0002025 88.1946 246.6659 1.00271889 04
| Epoch (UTC): | 25 May 2026 12:27:38 |
| Eccentricity: | 0.0002025 |
| inclination: | 0.0178° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 328.1582° |
| argument of perigee: | 88.1946° |
| revolutions per day: | 1.00271889 |
| mean anomaly at epoch: | 246.6659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|