View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62729U 26145.60980405 +.00000000 +00000-0 +88482-3 0 00002
2 62729 97.6389 323.4807 0008655 19.5207 340.6364 15.33748211 06
| Epoch (UTC): | 25 May 2026 14:38:07 |
| Eccentricity: | 0.0008655 |
| inclination: | 97.6389° |
| perigee height: | 459 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 323.4807° |
| argument of perigee: | 19.5207° |
| revolutions per day: | 15.33748211 |
| mean anomaly at epoch: | 340.6364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|