View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45703U 26144.68511818 +.00000000 +00000-0 +44602-3 0 00006
2 45703 53.0278 301.8327 0003974 0.2323 359.8695 15.71729975 01
| Epoch (UTC): | 24 May 2026 16:26:34 |
| Eccentricity: | 0.0003974 |
| inclination: | 53.0278° |
| perigee height: | 351 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 301.8327° |
| argument of perigee: | 0.2323° |
| revolutions per day: | 15.71729975 |
| mean anomaly at epoch: | 359.8695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|