View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68325U 26145.27648123 +.00000000 +00000-0 +90178-3 0 00006
2 68325 53.1601 348.8022 0001009 90.4737 269.6382 15.35420264 07
| Epoch (UTC): | 25 May 2026 06:38:07 |
| Eccentricity: | 0.0001009 |
| inclination: | 53.1601° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 348.8022° |
| argument of perigee: | 90.4737° |
| revolutions per day: | 15.35420264 |
| mean anomaly at epoch: | 269.6382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|