View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68933U 26145.38363825 +.00000000 +00000-0 -15822-3 0 00000
2 68933 51.8755 177.6779 0009146 51.5634 308.6171 15.34120501 08
| Epoch (UTC): | 25 May 2026 09:12:26 |
| Eccentricity: | 0.0009146 |
| inclination: | 51.8755° |
| perigee height: | 457 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 177.6779° |
| argument of perigee: | 51.5634° |
| revolutions per day: | 15.34120501 |
| mean anomaly at epoch: | 308.6171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|