View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59030U 26145.50583237 +.00000000 +00000-0 +42246-4 0 00003
2 59030 43.0042 313.4194 0001756 269.7708 90.2942 15.27567996 08
| Epoch (UTC): | 25 May 2026 12:08:23 |
| Eccentricity: | 0.0001756 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.4194° |
| argument of perigee: | 269.7708° |
| revolutions per day: | 15.27567996 |
| mean anomaly at epoch: | 90.2942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|