View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62008U 26145.38666741 +.00000000 +00000-0 +13191-2 0 00005
2 62008 53.1583 23.0005 0000950 80.9047 279.2079 15.69784675 09
| Epoch (UTC): | 25 May 2026 09:16:48 |
| Eccentricity: | 0.0000950 |
| inclination: | 53.1583° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 23.0005° |
| argument of perigee: | 80.9047° |
| revolutions per day: | 15.69784675 |
| mean anomaly at epoch: | 279.2079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|