View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28654U 05018A 24255.01443231 .00000778 00000-0 43797-3 0 9990
2 28654 98.8691 331.2512 0014438 176.1525 183.9761 14.13321556995382
| Epoch (UTC): | 11 September 2024 00:20:46 |
| Eccentricity: | 0.0014438 |
| inclination: | 98.8691° |
| perigee height: | 837 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 331.2512° |
| argument of perigee: | 176.1525° |
| revolutions per day: | 14.13321556 |
| mean anomaly at epoch: | 183.9761° |
| orbit number at epoch: | 99538 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|