View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67522U 26109.29352375 +.00000000 +00000-0 +12781-3 0 00001
2 67522 50.0075 207.1050 0000467 255.3513 104.7307 13.29325670 07
| Epoch (UTC): | 19 April 2026 07:02:40 |
| Eccentricity: | 0.0000467 |
| inclination: | 50.0075° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 207.1050° |
| argument of perigee: | 255.3513° |
| revolutions per day: | 13.29325670 |
| mean anomaly at epoch: | 104.7307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|