View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48331U 26145.61800442 +.00000000 +00000-0 +13322-2 0 00008
2 48331 53.1597 103.6335 0001559 107.6803 252.4368 15.31187373 06
| Epoch (UTC): | 25 May 2026 14:49:55 |
| Eccentricity: | 0.0001559 |
| inclination: | 53.1597° |
| perigee height: | 471 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 103.6335° |
| argument of perigee: | 107.6803° |
| revolutions per day: | 15.31187373 |
| mean anomaly at epoch: | 252.4368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|