View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58427U 26145.64143976 +.00000000 +00000-0 +10691-3 0 00007
2 58427 49.9598 49.4281 0011075 189.9649 170.1010 13.41482410 08
| Epoch (UTC): | 25 May 2026 15:23:40 |
| Eccentricity: | 0.0011075 |
| inclination: | 49.9598° |
| perigee height: | 1095 km |
| apogee height: | 1112 km |
| right ascension of ascending node: | 49.4281° |
| argument of perigee: | 189.9649° |
| revolutions per day: | 13.41482410 |
| mean anomaly at epoch: | 170.1010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|