View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32299U 26145.37079053 +.00000000 +00000-0 +00000-0 0 00000
2 32299 0.0175 310.1409 0002472 117.2420 313.8702 1.00274462 00
| Epoch (UTC): | 25 May 2026 08:53:56 |
| Eccentricity: | 0.0002472 |
| inclination: | 0.0175° |
| perigee height: | 35775 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 310.1409° |
| argument of perigee: | 117.2420° |
| revolutions per day: | 1.00274462 |
| mean anomaly at epoch: | 313.8702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|