View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 40074U 14037F 22176.63703109 .00001641 00000-0 19738-3 0 9990
2 40074 98.3816 57.7346 0003048 272.5257 87.5596 14.85430327431284
| Epoch (UTC): | 25 June 2022 15:17:19 |
| Eccentricity: | 0.0003048 |
| inclination: | 98.3816° |
| perigee height: | 610 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 57.7346° |
| argument of perigee: | 272.5257° |
| revolutions per day: | 14.85430327 |
| mean anomaly at epoch: | 87.5596° |
| orbit number at epoch: | 43128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|