View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37212U 26085.58076579 +.00000000 +00000-0 +00000-0 0 00006
2 37212 63.4563 100.7079 6788447 261.1970 22.6201 2.00595816 07
| Epoch (UTC): | 26 March 2026 13:56:18 |
| Eccentricity: | 0.6788447 |
| inclination: | 63.4563° |
| perigee height: | 2151 km |
| apogee height: | 38208 km |
| right ascension of ascending node: | 100.7079° |
| argument of perigee: | 261.1970° |
| revolutions per day: | 2.00595816 |
| mean anomaly at epoch: | 22.6201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|