View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26931U 01043C 23038.74965622 .00000360 00000-0 16854-3 0 9992
2 26931 67.0509 171.0178 0005921 282.6217 77.4222 14.30812884115066
| Epoch (UTC): | 07 February 2023 17:59:30 |
| Eccentricity: | 0.0005921 |
| inclination: | 67.0509° |
| perigee height: | 785 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 171.0178° |
| argument of perigee: | 282.6217° |
| revolutions per day: | 14.30812884 |
| mean anomaly at epoch: | 77.4222° |
| orbit number at epoch: | 11506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|