View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67525U 26145.50497205 +.00000000 +00000-0 +71423-4 0 00009
2 67525 50.0087 77.0248 0001087 35.6646 324.4298 13.29327378 08
| Epoch (UTC): | 25 May 2026 12:07:09 |
| Eccentricity: | 0.0001087 |
| inclination: | 50.0087° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 77.0248° |
| argument of perigee: | 35.6646° |
| revolutions per day: | 13.29327378 |
| mean anomaly at epoch: | 324.4298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|