View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68060U 26145.04318653 +.00000000 +00000-0 +53857-3 0 00002
2 68060 53.1575 53.4283 0000996 61.4730 298.6372 15.34393755 00
| Epoch (UTC): | 25 May 2026 01:02:11 |
| Eccentricity: | 0.0000996 |
| inclination: | 53.1575° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 53.4283° |
| argument of perigee: | 61.4730° |
| revolutions per day: | 15.34393755 |
| mean anomaly at epoch: | 298.6372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|