View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65827U 26145.12486300 +.00000000 +00000-0 +67011-3 0 00001
2 65827 53.1597 92.7640 0001134 78.4603 281.6527 15.34402392 09
| Epoch (UTC): | 25 May 2026 02:59:48 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.7640° |
| argument of perigee: | 78.4603° |
| revolutions per day: | 15.34402392 |
| mean anomaly at epoch: | 281.6527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|