View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45147U 26145.21862418 +.00000000 +00000-0 +25545-3 0 00008
2 45147 87.8854 40.8516 0001832 75.4483 284.6848 13.10377085 07
| Epoch (UTC): | 25 May 2026 05:14:49 |
| Eccentricity: | 0.0001832 |
| inclination: | 87.8854° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8516° |
| argument of perigee: | 75.4483° |
| revolutions per day: | 13.10377085 |
| mean anomaly at epoch: | 284.6848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|