View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68888U 26145.60161192 +.00000000 +00000-0 +88068-3 0 00008
2 68888 51.8778 351.6620 0006913 202.9460 157.1219 15.37352332 01
| Epoch (UTC): | 25 May 2026 14:26:19 |
| Eccentricity: | 0.0006913 |
| inclination: | 51.8778° |
| perigee height: | 449 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 351.6620° |
| argument of perigee: | 202.9460° |
| revolutions per day: | 15.37352332 |
| mean anomaly at epoch: | 157.1219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|