View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48330U 26145.29830133 +.00000000 +00000-0 +39322-1 0 00008
2 48330 53.1584 105.1539 0007521 286.1033 73.9141 15.33818289 01
| Epoch (UTC): | 25 May 2026 07:09:33 |
| Eccentricity: | 0.0007521 |
| inclination: | 53.1584° |
| perigee height: | 459 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 105.1539° |
| argument of perigee: | 286.1033° |
| revolutions per day: | 15.33818289 |
| mean anomaly at epoch: | 73.9141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|