View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52304U 26145.61480703 +.00000000 +00000-0 +45663-4 0 00002
2 52304 53.2122 103.7909 0001168 82.9603 277.1522 15.08838369 01
| Epoch (UTC): | 25 May 2026 14:45:19 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 103.7909° |
| argument of perigee: | 82.9603° |
| revolutions per day: | 15.08838369 |
| mean anomaly at epoch: | 277.1522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|