View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63209U 26145.61803705 +.00000000 +00000-0 +65717-3 0 00000
2 63209 97.4512 232.1623 0006856 163.5647 196.5826 15.46889501 00
| Epoch (UTC): | 25 May 2026 14:49:58 |
| Eccentricity: | 0.0006856 |
| inclination: | 97.4512° |
| perigee height: | 421 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 232.1623° |
| argument of perigee: | 163.5647° |
| revolutions per day: | 15.46889501 |
| mean anomaly at epoch: | 196.5826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|