View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65442U 26145.33710738 +.00000000 +00000-0 +29068-3 0 00002
2 65442 97.4487 359.6007 0001914 88.5353 271.6093 15.05657345 08
| Epoch (UTC): | 25 May 2026 08:05:26 |
| Eccentricity: | 0.0001914 |
| inclination: | 97.4487° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.6007° |
| argument of perigee: | 88.5353° |
| revolutions per day: | 15.05657345 |
| mean anomaly at epoch: | 271.6093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|