View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13121U 26103.24861990 +.00000000 +00000-0 +13179-3 0 00006
2 13121 81.1903 356.8984 0008587 148.8829 211.2917 15.28853806 02
| Epoch (UTC): | 13 April 2026 05:58:00 |
| Eccentricity: | 0.0008587 |
| inclination: | 81.1903° |
| perigee height: | 473 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 356.8984° |
| argument of perigee: | 148.8829° |
| revolutions per day: | 15.28853806 |
| mean anomaly at epoch: | 211.2917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|