View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 22565U 93016A 25197.72007813 -.00000301 00000-0 -13640-3 0 9994
2 22565 70.7864 302.5247 0005815 22.4715 337.6659 14.12446158665986
| Epoch (UTC): | 16 July 2025 17:16:54 |
| Eccentricity: | 0.0005815 |
| inclination: | 70.7864° |
| perigee height: | 847 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 302.5247° |
| argument of perigee: | 22.4715° |
| revolutions per day: | 14.12446158 |
| mean anomaly at epoch: | 337.6659° |
| orbit number at epoch: | 66598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|