View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61661U 26145.10597568 +.00000000 +00000-0 +15797-3 0 00004
2 61661 53.1611 96.2489 0001313 111.4328 248.6813 15.30199774 03
| Epoch (UTC): | 25 May 2026 02:32:36 |
| Eccentricity: | 0.0001313 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 96.2489° |
| argument of perigee: | 111.4328° |
| revolutions per day: | 15.30199774 |
| mean anomaly at epoch: | 248.6813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|