View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 25919U 99051A 24283.86932996 .00007988 00000-0 76868-3 0 9991
2 25919 98.2149 135.2453 0008220 76.9881 283.2254 14.93244247346947
| Epoch (UTC): | 09 October 2024 20:51:50 |
| Eccentricity: | 0.0008220 |
| inclination: | 98.2149° |
| perigee height: | 582 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 135.2453° |
| argument of perigee: | 76.9881° |
| revolutions per day: | 14.93244247 |
| mean anomaly at epoch: | 283.2254° |
| orbit number at epoch: | 34694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|