View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59751U 26145.37983361 +.00000000 +00000-0 +58703-4 0 00005
2 59751 43.0018 109.9780 0000944 263.1968 96.8776 15.27580363 04
| Epoch (UTC): | 25 May 2026 09:06:57 |
| Eccentricity: | 0.0000944 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 109.9780° |
| argument of perigee: | 263.1968° |
| revolutions per day: | 15.27580363 |
| mean anomaly at epoch: | 96.8776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|