View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58914U 26145.36236852 +.00000000 +00000-0 +15240-3 0 00008
2 58914 49.9942 99.6947 0010062 271.7859 88.1927 14.83152778 09
| Epoch (UTC): | 25 May 2026 08:41:48 |
| Eccentricity: | 0.0010062 |
| inclination: | 49.9942° |
| perigee height: | 612 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 99.6947° |
| argument of perigee: | 271.7859° |
| revolutions per day: | 14.83152778 |
| mean anomaly at epoch: | 88.1927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|