View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51745U 26145.53844959 +.00000000 +00000-0 +26504-4 0 00001
2 51745 53.2120 334.1330 0001232 78.0928 282.0202 15.08835861 07
| Epoch (UTC): | 25 May 2026 12:55:22 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.1330° |
| argument of perigee: | 78.0928° |
| revolutions per day: | 15.08835861 |
| mean anomaly at epoch: | 282.0202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|