View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57693U 26145.66657692 +.00000000 +00000-0 +58793-3 0 00003
2 57693 53.0075 282.4792 0001806 62.3532 297.7629 14.82515559 09
| Epoch (UTC): | 25 May 2026 15:59:52 |
| Eccentricity: | 0.0001806 |
| inclination: | 53.0075° |
| perigee height: | 620 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 282.4792° |
| argument of perigee: | 62.3532° |
| revolutions per day: | 14.82515559 |
| mean anomaly at epoch: | 297.7629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|