View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26061U 00004A 22222.17980313 .00000233 00000-0 89472-4 0 9993
2 26061 100.1997 290.0310 0032774 281.4819 78.2685 14.41723001184085
| Epoch (UTC): | 10 August 2022 04:18:54 |
| Eccentricity: | 0.0032774 |
| inclination: | 100.1997° |
| perigee height: | 729 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 290.0310° |
| argument of perigee: | 281.4819° |
| revolutions per day: | 14.41723001 |
| mean anomaly at epoch: | 78.2685° |
| orbit number at epoch: | 18408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|