View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68050U 26145.45924787 +.00000000 +00000-0 +49806-3 0 00006
2 68050 53.1596 51.7477 0001134 98.8613 261.2518 15.34404136 01
| Epoch (UTC): | 25 May 2026 11:01:19 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 51.7477° |
| argument of perigee: | 98.8613° |
| revolutions per day: | 15.34404136 |
| mean anomaly at epoch: | 261.2518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|