View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45153U 26145.46597084 +.00000000 +00000-0 +19602-2 0 00002
2 45153 87.8853 40.8109 0001777 77.6785 282.4542 13.10373861 03
| Epoch (UTC): | 25 May 2026 11:10:59 |
| Eccentricity: | 0.0001777 |
| inclination: | 87.8853° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8109° |
| argument of perigee: | 77.6785° |
| revolutions per day: | 13.10373861 |
| mean anomaly at epoch: | 282.4542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|