View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44453U 26144.29029912 +.00000000 +00000-0 +00000-0 0 00004
2 44453 63.1160 53.8420 7069462 274.8017 14.7796 2.00604462 02
| Epoch (UTC): | 24 May 2026 06:58:01 |
| Eccentricity: | 0.7069462 |
| inclination: | 63.1160° |
| perigee height: | 1404 km |
| apogee height: | 38953 km |
| right ascension of ascending node: | 53.8420° |
| argument of perigee: | 274.8017° |
| revolutions per day: | 2.00604462 |
| mean anomaly at epoch: | 14.7796° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|