View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 35459U 93036ALD 24355.67147916 .00001728 00000-0 59640-3 0 9992
2 35459 73.8720 130.5171 0016408 150.3136 209.8951 14.36547943532326
| Epoch (UTC): | 20 December 2024 16:06:55 |
| Eccentricity: | 0.0016408 |
| inclination: | 73.8720° |
| perigee height: | 758 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 130.5171° |
| argument of perigee: | 150.3136° |
| revolutions per day: | 14.36547943 |
| mean anomaly at epoch: | 209.8951° |
| orbit number at epoch: | 53232 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|