View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 40380U 15003E 24182.35509181 .14513438 37056-5 19265-3 0 9994
2 40380 99.0710 214.6222 0010155 269.4194 90.5941 16.48902700521563
| Epoch (UTC): | 30 June 2024 08:31:19 |
| Eccentricity: | 0.0010155 |
| inclination: | 99.0710° |
| perigee height: | 135 km |
| apogee height: | 149 km |
| right ascension of ascending node: | 214.6222° |
| argument of perigee: | 269.4194° |
| revolutions per day: | 16.48902700 |
| mean anomaly at epoch: | 90.5941° |
| orbit number at epoch: | 52156 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|