View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 23855U 96026A 22277.80536195 0.00000000 00000-0 00000-0 0 06
2 23855 8.5591 353.3250 0359634 283.9458 76.0545 1.00270000 00
| Epoch (UTC): | 04 October 2022 19:19:43 |
| Eccentricity: | 0.0359634 |
| inclination: | 8.5591° |
| perigee height: | 34270 km |
| apogee height: | 37303 km |
| right ascension of ascending node: | 353.3250° |
| argument of perigee: | 283.9458° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 76.0545° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|