View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55379U 26145.27214557 +.00000000 +00000-0 +13449-4 0 00008
2 55379 43.0050 245.7691 0002023 277.1744 82.8877 15.27577680 04
| Epoch (UTC): | 25 May 2026 06:31:53 |
| Eccentricity: | 0.0002023 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 245.7691° |
| argument of perigee: | 277.1744° |
| revolutions per day: | 15.27577680 |
| mean anomaly at epoch: | 82.8877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|