View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 40042U 14033AJ 25073.43503229 .00030614 00000-0 16451-2 0 9999
2 40042 98.0999 57.7501 0008094 309.6762 50.3753 15.14815966583572
| Epoch (UTC): | 14 March 2025 10:26:26 |
| Eccentricity: | 0.0008094 |
| inclination: | 98.0999° |
| perigee height: | 516 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 57.7501° |
| argument of perigee: | 309.6762° |
| revolutions per day: | 15.14815966 |
| mean anomaly at epoch: | 50.3753° |
| orbit number at epoch: | 58357 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|