View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48311U 26145.55230593 +.00000000 +00000-0 +28809-4 0 00001
2 48311 53.1594 91.1709 0000915 106.6281 253.4821 15.31704507 00
| Epoch (UTC): | 25 May 2026 13:15:19 |
| Eccentricity: | 0.0000915 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 91.1709° |
| argument of perigee: | 106.6281° |
| revolutions per day: | 15.31704507 |
| mean anomaly at epoch: | 253.4821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|