View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00552U 26101.37234838 +.00000000 +00000-0 +75914-3 0 00002
2 00552 67.7360 210.5606 0094592 51.0808 309.8668 13.99484780 07
| Epoch (UTC): | 11 April 2026 08:56:10 |
| Eccentricity: | 0.0094592 |
| inclination: | 67.7360° |
| perigee height: | 827 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 210.5606° |
| argument of perigee: | 51.0808° |
| revolutions per day: | 13.99484780 |
| mean anomaly at epoch: | 309.8668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|