View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00059U 60013B 25166.41134374 .00000102 00000-0 19808-4 0 9994
2 00059 28.2459 208.1339 0189043 116.4675 245.5393 13.53139369193453
| Epoch (UTC): | 15 June 2025 09:52:20 |
| Eccentricity: | 0.0189043 |
| inclination: | 28.2459° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 208.1339° |
| argument of perigee: | 116.4675° |
| revolutions per day: | 13.53139369 |
| mean anomaly at epoch: | 245.5393° |
| orbit number at epoch: | 19345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|