View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 09662U 77002B 25198.34904940 .00000134 00000-0 79410-4 0 9990
2 09662 81.2763 132.7855 0053041 113.7598 246.9143 14.01252427479737
| Epoch (UTC): | 17 July 2025 08:22:37 |
| Eccentricity: | 0.0053041 |
| inclination: | 81.2763° |
| perigee height: | 851 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 132.7855° |
| argument of perigee: | 113.7598° |
| revolutions per day: | 14.01252427 |
| mean anomaly at epoch: | 246.9143° |
| orbit number at epoch: | 47973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|