View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59299U 26145.45060939 +.00000000 +00000-0 -35413-4 0 00002
2 59299 43.0009 150.3103 0001037 263.6440 96.4293 15.27580998 08
| Epoch (UTC): | 25 May 2026 10:48:52 |
| Eccentricity: | 0.0001037 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.3103° |
| argument of perigee: | 263.6440° |
| revolutions per day: | 15.27580998 |
| mean anomaly at epoch: | 96.4293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|