View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54646U 26145.51650469 +.00000000 +00000-0 +13868-3 0 00001
2 54646 87.9260 248.4789 0002232 95.1759 264.9630 13.21825288 06
| Epoch (UTC): | 25 May 2026 12:23:46 |
| Eccentricity: | 0.0002232 |
| inclination: | 87.9260° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4789° |
| argument of perigee: | 95.1759° |
| revolutions per day: | 13.21825288 |
| mean anomaly at epoch: | 264.9630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|