View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43073U 26145.50850693 +.00000000 +00000-0 +99428-5 0 00001
2 43073 86.3963 331.7601 0002122 83.0532 277.0905 14.34218007 03
| Epoch (UTC): | 25 May 2026 12:12:14 |
| Eccentricity: | 0.0002122 |
| inclination: | 86.3963° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.7601° |
| argument of perigee: | 83.0532° |
| revolutions per day: | 14.34218007 |
| mean anomaly at epoch: | 277.0905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|