View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48058U 26145.45785852 +.00000000 +00000-0 -49835-3 0 00003
2 48058 87.8950 324.7500 0001981 95.1856 264.9499 13.13469269 05
| Epoch (UTC): | 25 May 2026 10:59:18 |
| Eccentricity: | 0.0001981 |
| inclination: | 87.8950° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7500° |
| argument of perigee: | 95.1856° |
| revolutions per day: | 13.13469269 |
| mean anomaly at epoch: | 264.9499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|