View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48274U 26110.34681916 +.00000000 +00000-0 +20498-3 0 00002
2 48274 41.4648 314.3083 0006488 240.5920 119.4272 15.62604461 05
| Epoch (UTC): | 20 April 2026 08:19:25 |
| Eccentricity: | 0.0006488 |
| inclination: | 41.4648° |
| perigee height: | 376 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 314.3083° |
| argument of perigee: | 240.5920° |
| revolutions per day: | 15.62604461 |
| mean anomaly at epoch: | 119.4272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|