View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 36938U 87011S 24355.53332797 .00001781 00000-0 62963-3 0 9990
2 36938 65.0085 286.1160 0020221 253.5903 106.2961 14.37201946824133
| Epoch (UTC): | 20 December 2024 12:47:59 |
| Eccentricity: | 0.0020221 |
| inclination: | 65.0085° |
| perigee height: | 753 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 286.1160° |
| argument of perigee: | 253.5903° |
| revolutions per day: | 14.37201946 |
| mean anomaly at epoch: | 106.2961° |
| orbit number at epoch: | 82413 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|