View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25319U 98026A 24358.00002410 .00000976 00000-0 30024-3 0 9998
2 25319 86.4000 169.8052 0000981 187.5155 172.6029 14.40602536397930
| Epoch (UTC): | 23 December 2024 00:00:02 |
| Eccentricity: | 0.0000981 |
| inclination: | 86.4000° |
| perigee height: | 756 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 169.8052° |
| argument of perigee: | 187.5155° |
| revolutions per day: | 14.40602536 |
| mean anomaly at epoch: | 172.6029° |
| orbit number at epoch: | 39793 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|