View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67523U 26145.52161838 +.00000000 +00000-0 +76876-4 0 00006
2 67523 50.0053 77.0701 0000878 26.3908 333.7008 13.29328922 06
| Epoch (UTC): | 25 May 2026 12:31:07 |
| Eccentricity: | 0.0000878 |
| inclination: | 50.0053° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 77.0701° |
| argument of perigee: | 26.3908° |
| revolutions per day: | 13.29328922 |
| mean anomaly at epoch: | 333.7008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|