View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68291U 26145.27830598 +.00000000 +00000-0 +24094-3 0 00001
2 68291 50.2822 98.0725 0016094 155.8064 204.3644 14.99982895 04
| Epoch (UTC): | 25 May 2026 06:40:45 |
| Eccentricity: | 0.0016094 |
| inclination: | 50.2822° |
| perigee height: | 556 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 98.0725° |
| argument of perigee: | 155.8064° |
| revolutions per day: | 14.99982895 |
| mean anomaly at epoch: | 204.3644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|