View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29052U 06011F 25132.24004876 .00000509 00000-0 20679-3 0 9991
2 29052 72.0306 121.7617 0037905 141.3094 219.0770 14.31147077996295
| Epoch (UTC): | 12 May 2025 05:45:40 |
| Eccentricity: | 0.0037905 |
| inclination: | 72.0306° |
| perigee height: | 761 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 121.7617° |
| argument of perigee: | 141.3094° |
| revolutions per day: | 14.31147077 |
| mean anomaly at epoch: | 219.0770° |
| orbit number at epoch: | 99629 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|