View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29092U 06015A 25191.61786139 .00000507 00000-0 62561-4 0 9999
2 29092 97.7726 215.1549 0001430 91.5801 268.5579 14.86967666 39037
| Epoch (UTC): | 10 July 2025 14:49:43 |
| Eccentricity: | 0.0001430 |
| inclination: | 97.7726° |
| perigee height: | 606 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 215.1549° |
| argument of perigee: | 91.5801° |
| revolutions per day: | 14.86967666 |
| mean anomaly at epoch: | 268.5579° |
| orbit number at epoch: | 3903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|