View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26548U 26105.95447931 +.00000000 +00000-0 +90382-4 0 00000
2 26548 64.5464 323.9465 0039114 297.8567 61.8587 15.01375383 01
| Epoch (UTC): | 15 April 2026 22:54:27 |
| Eccentricity: | 0.0039114 |
| inclination: | 64.5464° |
| perigee height: | 536 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 323.9465° |
| argument of perigee: | 297.8567° |
| revolutions per day: | 15.01375383 |
| mean anomaly at epoch: | 61.8587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|