View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45245U 26145.53939269 +.00000000 +00000-0 +00000-0 0 00007
2 45245 5.3929 356.6687 0003079 52.6949 163.9496 1.00271936 02
| Epoch (UTC): | 25 May 2026 12:56:43 |
| Eccentricity: | 0.0003079 |
| inclination: | 5.3929° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 356.6687° |
| argument of perigee: | 52.6949° |
| revolutions per day: | 1.00271936 |
| mean anomaly at epoch: | 163.9496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|