View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61697U 26145.32911366 +.00000000 +00000-0 +13603-4 0 00008
2 61697 53.1581 8.2380 0001058 90.2390 269.8749 15.69709462 06
| Epoch (UTC): | 25 May 2026 07:53:55 |
| Eccentricity: | 0.0001058 |
| inclination: | 53.1581° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 8.2380° |
| argument of perigee: | 90.2390° |
| revolutions per day: | 15.69709462 |
| mean anomaly at epoch: | 269.8749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|