View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56923U 26145.60803066 +.00000000 +00000-0 +14381-3 0 00005
2 56923 43.0028 356.1224 0001240 253.9693 106.1022 15.27595654 02
| Epoch (UTC): | 25 May 2026 14:35:33 |
| Eccentricity: | 0.0001240 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.1224° |
| argument of perigee: | 253.9693° |
| revolutions per day: | 15.27595654 |
| mean anomaly at epoch: | 106.1022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|