View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61595U 26145.60180745 +.00000000 +00000-0 -63398-4 0 00002
2 61595 87.9147 10.3696 0002131 96.5652 263.5723 13.17649911 09
| Epoch (UTC): | 25 May 2026 14:26:36 |
| Eccentricity: | 0.0002131 |
| inclination: | 87.9147° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3696° |
| argument of perigee: | 96.5652° |
| revolutions per day: | 13.17649911 |
| mean anomaly at epoch: | 263.5723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|