View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48274U 26138.46988833 +.00000000 +00000-0 +12053-3 0 00001
2 48274 41.4668 142.7157 0007478 254.3964 105.6049 15.60652819 00
| Epoch (UTC): | 18 May 2026 11:16:38 |
| Eccentricity: | 0.0007478 |
| inclination: | 41.4668° |
| perigee height: | 381 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 142.7157° |
| argument of perigee: | 254.3964° |
| revolutions per day: | 15.60652819 |
| mean anomaly at epoch: | 105.6049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|