View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60282U 26145.05260941 +.00000000 +00000-0 +15237-4 0 00008
2 60282 53.1605 57.6085 0001134 86.2205 273.8926 15.30195126 03
| Epoch (UTC): | 25 May 2026 01:15:45 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.6085° |
| argument of perigee: | 86.2205° |
| revolutions per day: | 15.30195126 |
| mean anomaly at epoch: | 273.8926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|