View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29051U 06011E 25318.42426899 .00001047 00000-0 40196-3 0 9993
2 29051 72.0055 21.1440 0063927 103.8458 256.9803 14.31293820 24536
| Epoch (UTC): | 14 November 2025 10:10:56 |
| Eccentricity: | 0.0063927 |
| inclination: | 72.0055° |
| perigee height: | 741 km |
| apogee height: | 833 km |
| right ascension of ascending node: | 21.1440° |
| argument of perigee: | 103.8458° |
| revolutions per day: | 14.31293820 |
| mean anomaly at epoch: | 256.9803° |
| orbit number at epoch: | 2453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|