View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48282U 26145.53522028 +.00000000 +00000-0 +36372-3 0 00006
2 48282 53.1604 78.0263 0001097 93.7127 266.4000 15.31722007 03
| Epoch (UTC): | 25 May 2026 12:50:43 |
| Eccentricity: | 0.0001097 |
| inclination: | 53.1604° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 78.0263° |
| argument of perigee: | 93.7127° |
| revolutions per day: | 15.31722007 |
| mean anomaly at epoch: | 266.4000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|