View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68086U 26145.53372255 +.00000000 +00000-0 +42956-3 0 00000
2 68086 53.1579 179.3957 0001277 53.7730 306.3390 15.34406808 06
| Epoch (UTC): | 25 May 2026 12:48:33 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.1579° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 179.3957° |
| argument of perigee: | 53.7730° |
| revolutions per day: | 15.34406808 |
| mean anomaly at epoch: | 306.3390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|