View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46265U 26145.61880100 +.00000000 +00000-0 +97128-4 0 00009
2 46265 97.8894 331.7896 0001503 85.5575 274.5809 14.82151759 09
| Epoch (UTC): | 25 May 2026 14:51:04 |
| Eccentricity: | 0.0001503 |
| inclination: | 97.8894° |
| perigee height: | 621 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 331.7896° |
| argument of perigee: | 85.5575° |
| revolutions per day: | 14.82151759 |
| mean anomaly at epoch: | 274.5809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|