View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54869U 26145.11458412 +.00000000 +00000-0 +12872-4 0 00003
2 54869 43.0061 50.4111 0001296 268.2368 91.8336 15.27572741 04
| Epoch (UTC): | 25 May 2026 02:45:00 |
| Eccentricity: | 0.0001296 |
| inclination: | 43.0061° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 50.4111° |
| argument of perigee: | 268.2368° |
| revolutions per day: | 15.27572741 |
| mean anomaly at epoch: | 91.8336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|