View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13242U 26088.07563875 +.00000000 +00000-0 +10177-3 0 00009
2 13242 74.0427 225.7013 0024550 356.1409 3.9551 14.37361681 05
| Epoch (UTC): | 29 March 2026 01:48:55 |
| Eccentricity: | 0.0024550 |
| inclination: | 74.0427° |
| perigee height: | 750 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 225.7013° |
| argument of perigee: | 356.1409° |
| revolutions per day: | 14.37361681 |
| mean anomaly at epoch: | 3.9551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|