View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26069U 00006A 25340.31358142 .00000145 00000-0 10166-3 0 9997
2 26069 70.9948 355.8007 0012978 228.7374 131.2631 14.13850785596694
| Epoch (UTC): | 06 December 2025 07:31:33 |
| Eccentricity: | 0.0012978 |
| inclination: | 70.9948° |
| perigee height: | 837 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 355.8007° |
| argument of perigee: | 228.7374° |
| revolutions per day: | 14.13850785 |
| mean anomaly at epoch: | 131.2631° |
| orbit number at epoch: | 59669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|