View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68932U 26145.49804804 +.00000000 +00000-0 +61976-3 0 00008
2 68932 51.8756 176.9476 0003658 73.2971 286.8416 15.35345519 09
| Epoch (UTC): | 25 May 2026 11:57:11 |
| Eccentricity: | 0.0003658 |
| inclination: | 51.8756° |
| perigee height: | 457 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 176.9476° |
| argument of perigee: | 73.2971° |
| revolutions per day: | 15.35345519 |
| mean anomaly at epoch: | 286.8416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|