View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27432U 02024C 25196.92073894 .00000015 00000-0 30945-4 0 9992
2 27432 98.9216 246.0101 0049703 336.2495 197.1425 14.14491053195842
| Epoch (UTC): | 15 July 2025 22:05:51 |
| Eccentricity: | 0.0049703 |
| inclination: | 98.9216° |
| perigee height: | 808 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 246.0101° |
| argument of perigee: | 336.2495° |
| revolutions per day: | 14.14491053 |
| mean anomaly at epoch: | 197.1425° |
| orbit number at epoch: | 19584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|