View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 60235U 24128A 24283.40509385 .00011222 00000-0 10051-2 0 9993
2 60235 61.9961 205.9750 0022252 327.3325 32.6385 14.96039581 13698
| Epoch (UTC): | 09 October 2024 09:43:20 |
| Eccentricity: | 0.0022252 |
| inclination: | 61.9961° |
| perigee height: | 563 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 205.9750° |
| argument of perigee: | 327.3325° |
| revolutions per day: | 14.96039581 |
| mean anomaly at epoch: | 32.6385° |
| orbit number at epoch: | 1369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|