View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53203U 26145.40531073 +.00000000 +00000-0 +64474-5 0 00007
2 53203 97.4524 206.4721 0001556 114.9747 245.1642 15.05651396 03
| Epoch (UTC): | 25 May 2026 09:43:38 |
| Eccentricity: | 0.0001556 |
| inclination: | 97.4524° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.4721° |
| argument of perigee: | 114.9747° |
| revolutions per day: | 15.05651396 |
| mean anomaly at epoch: | 245.1642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|