View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53933U 26145.50485238 +.00000000 +00000-0 +17773-4 0 00008
2 53933 53.2132 319.1405 0001191 87.3854 272.7274 15.08834026 09
| Epoch (UTC): | 25 May 2026 12:06:59 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 319.1405° |
| argument of perigee: | 87.3854° |
| revolutions per day: | 15.08834026 |
| mean anomaly at epoch: | 272.7274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|