View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68821U 26145.55130424 +.00000000 +00000-0 +16551-2 0 00000
2 68821 97.2845 352.2383 0001480 90.2089 269.9346 15.75272511 04
| Epoch (UTC): | 25 May 2026 13:13:52 |
| Eccentricity: | 0.0001480 |
| inclination: | 97.2845° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2383° |
| argument of perigee: | 90.2089° |
| revolutions per day: | 15.75272511 |
| mean anomaly at epoch: | 269.9346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|