View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 69075U 26145.52264079 +.00000000 +00000-0 +53023-4 0 00000
2 69075 88.9868 344.2038 0003396 156.7009 203.4339 14.26565178 08
| Epoch (UTC): | 25 May 2026 12:32:36 |
| Eccentricity: | 0.0003396 |
| inclination: | 88.9868° |
| perigee height: | 801 km |
| apogee height: | 806 km |
| right ascension of ascending node: | 344.2038° |
| argument of perigee: | 156.7009° |
| revolutions per day: | 14.26565178 |
| mean anomaly at epoch: | 203.4339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|