View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48303U 26145.55694079 +.00000000 +00000-0 +50854-4 0 00000
2 48303 53.1598 90.9371 0001218 88.9966 271.1175 15.31702839 01
| Epoch (UTC): | 25 May 2026 13:21:59 |
| Eccentricity: | 0.0001218 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 90.9371° |
| argument of perigee: | 88.9966° |
| revolutions per day: | 15.31702839 |
| mean anomaly at epoch: | 271.1175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|