View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62696U 26145.18041926 +.00000000 +00000-0 +60895-3 0 00002
2 62696 97.6904 226.9654 0001964 178.8174 181.3056 15.02085933 06
| Epoch (UTC): | 25 May 2026 04:19:48 |
| Eccentricity: | 0.0001964 |
| inclination: | 97.6904° |
| perigee height: | 559 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 226.9654° |
| argument of perigee: | 178.8174° |
| revolutions per day: | 15.02085933 |
| mean anomaly at epoch: | 181.3056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|