View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45673U 26145.40098523 +.00000000 +00000-0 +97435-3 0 00008
2 45673 53.0415 34.4389 0005677 105.9889 254.1751 15.63482263 06
| Epoch (UTC): | 25 May 2026 09:37:25 |
| Eccentricity: | 0.0005677 |
| inclination: | 53.0415° |
| perigee height: | 374 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 34.4389° |
| argument of perigee: | 105.9889° |
| revolutions per day: | 15.63482263 |
| mean anomaly at epoch: | 254.1751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|