View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62694U 26145.13931947 +.00000000 +00000-0 +15745-3 0 00000
2 62694 97.7027 224.0103 0004681 109.1460 251.0268 14.95045551 06
| Epoch (UTC): | 25 May 2026 03:20:37 |
| Eccentricity: | 0.0004681 |
| inclination: | 97.7027° |
| perigee height: | 579 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 224.0103° |
| argument of perigee: | 109.1460° |
| revolutions per day: | 14.95045551 |
| mean anomaly at epoch: | 251.0268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|