View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55149U 26145.28963705 +.00000000 +00000-0 +55129-4 0 00001
2 55149 87.9158 340.0275 0002023 100.4400 259.6960 13.18688127 03
| Epoch (UTC): | 25 May 2026 06:57:04 |
| Eccentricity: | 0.0002023 |
| inclination: | 87.9158° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0275° |
| argument of perigee: | 100.4400° |
| revolutions per day: | 13.18688127 |
| mean anomaly at epoch: | 259.6960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|