View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68419U 26144.85106531 +.00000000 +00000-0 +12765-3 0 00001
2 68419 97.4528 103.7073 0002295 42.5378 317.6033 15.18744408 08
| Epoch (UTC): | 24 May 2026 20:25:32 |
| Eccentricity: | 0.0002295 |
| inclination: | 97.4528° |
| perigee height: | 508 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 103.7073° |
| argument of perigee: | 42.5378° |
| revolutions per day: | 15.18744408 |
| mean anomaly at epoch: | 317.6033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|