View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26064U 00004D 23081.09979243 .00000213 00000-0 91979-4 0 9994
2 26064 100.2039 137.1355 0037988 154.4640 205.8428 14.36411916213101
| Epoch (UTC): | 22 March 2023 02:23:42 |
| Eccentricity: | 0.0037988 |
| inclination: | 100.2039° |
| perigee height: | 743 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 137.1355° |
| argument of perigee: | 154.4640° |
| revolutions per day: | 14.36411916 |
| mean anomaly at epoch: | 205.8428° |
| orbit number at epoch: | 21310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|