View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68170U 26145.34992958 +.00000000 +00000-0 +11127-2 0 00006
2 68170 53.1587 270.4294 0000954 113.3111 246.7994 15.38858691 05
| Epoch (UTC): | 25 May 2026 08:23:53 |
| Eccentricity: | 0.0000954 |
| inclination: | 53.1587° |
| perigee height: | 449 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 270.4294° |
| argument of perigee: | 113.3111° |
| revolutions per day: | 15.38858691 |
| mean anomaly at epoch: | 246.7994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|