View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68234U 26145.40689718 +.00000000 +00000-0 +87685-3 0 00004
2 68234 53.1590 298.7226 0001623 81.6726 278.4464 15.42186643 01
| Epoch (UTC): | 25 May 2026 09:45:55 |
| Eccentricity: | 0.0001623 |
| inclination: | 53.1590° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 298.7226° |
| argument of perigee: | 81.6726° |
| revolutions per day: | 15.42186643 |
| mean anomaly at epoch: | 278.4464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|