View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55382U 26145.53754542 +.00000000 +00000-0 +77346-4 0 00000
2 55382 43.0040 244.3228 0001630 269.2568 90.8097 15.27572619 07
| Epoch (UTC): | 25 May 2026 12:54:03 |
| Eccentricity: | 0.0001630 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 244.3228° |
| argument of perigee: | 269.2568° |
| revolutions per day: | 15.27572619 |
| mean anomaly at epoch: | 90.8097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|