View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48292U 26145.54450449 +.00000000 +00000-0 +45968-4 0 00007
2 48292 53.1610 77.7948 0001190 89.3942 270.7195 15.31705303 00
| Epoch (UTC): | 25 May 2026 13:04:05 |
| Eccentricity: | 0.0001190 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 77.7948° |
| argument of perigee: | 89.3942° |
| revolutions per day: | 15.31705303 |
| mean anomaly at epoch: | 270.7195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|