View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65913U 26145.48063215 +.00000000 +00000-0 +28424-3 0 00007
2 65913 53.1582 169.1025 0001093 86.8550 273.2576 15.30212598 07
| Epoch (UTC): | 25 May 2026 11:32:06 |
| Eccentricity: | 0.0001093 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.1025° |
| argument of perigee: | 86.8550° |
| revolutions per day: | 15.30212598 |
| mean anomaly at epoch: | 273.2576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|