View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53189U 26145.44961076 +.00000000 +00000-0 -35056-4 0 00008
2 53189 97.4487 206.4625 0001752 100.8278 259.3147 15.05658896 07
| Epoch (UTC): | 25 May 2026 10:47:26 |
| Eccentricity: | 0.0001752 |
| inclination: | 97.4487° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.4625° |
| argument of perigee: | 100.8278° |
| revolutions per day: | 15.05658896 |
| mean anomaly at epoch: | 259.3147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|