View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28892U 05043C 24357.86716385 .00004059 00000-0 69419-3 0 9996
2 28892 98.2327 134.9218 0015506 122.5846 237.6858 14.69339981 22180
| Epoch (UTC): | 22 December 2024 20:48:42 |
| Eccentricity: | 0.0015506 |
| inclination: | 98.2327° |
| perigee height: | 652 km |
| apogee height: | 674 km |
| right ascension of ascending node: | 134.9218° |
| argument of perigee: | 122.5846° |
| revolutions per day: | 14.69339981 |
| mean anomaly at epoch: | 237.6858° |
| orbit number at epoch: | 2218 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|