View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43065U 26145.43456367 +.00000000 +00000-0 +60914-4 0 00001
2 43065 98.6280 219.3764 0001224 97.4498 262.6822 14.27283895 02
| Epoch (UTC): | 25 May 2026 10:25:46 |
| Eccentricity: | 0.0001224 |
| inclination: | 98.6280° |
| perigee height: | 800 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 219.3764° |
| argument of perigee: | 97.4498° |
| revolutions per day: | 14.27283895 |
| mean anomaly at epoch: | 262.6822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|