View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26094U 00004M 25133.56622045 .00000889 00000-0 26318-3 0 9997
2 26094 100.1860 64.5002 0031234 250.7268 109.0538 14.46378028327448
| Epoch (UTC): | 13 May 2025 13:35:21 |
| Eccentricity: | 0.0031234 |
| inclination: | 100.1860° |
| perigee height: | 715 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 64.5002° |
| argument of perigee: | 250.7268° |
| revolutions per day: | 14.46378028 |
| mean anomaly at epoch: | 109.0538° |
| orbit number at epoch: | 32744 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|