View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52337U 26145.48968455 +.00000000 +00000-0 -15058-4 0 00004
2 52337 53.2143 224.3525 0001212 91.1458 268.9673 15.08838632 02
| Epoch (UTC): | 25 May 2026 11:45:08 |
| Eccentricity: | 0.0001212 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 224.3525° |
| argument of perigee: | 91.1458° |
| revolutions per day: | 15.08838632 |
| mean anomaly at epoch: | 268.9673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|