View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53193U 26145.12705477 +.00000000 +00000-0 -53399-3 0 00008
2 53193 97.4498 205.0598 0000614 224.5226 135.5952 15.05671161 00
| Epoch (UTC): | 25 May 2026 03:02:57 |
| Eccentricity: | 0.0000614 |
| inclination: | 97.4498° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 205.0598° |
| argument of perigee: | 224.5226° |
| revolutions per day: | 15.05671161 |
| mean anomaly at epoch: | 135.5952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|