View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53047U 26145.43719345 +.00000000 +00000-0 +53360-3 0 00006
2 53047 97.4444 325.3786 0001009 136.1151 224.0156 15.05617055 00
| Epoch (UTC): | 25 May 2026 10:29:33 |
| Eccentricity: | 0.0001009 |
| inclination: | 97.4444° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.3786° |
| argument of perigee: | 136.1151° |
| revolutions per day: | 15.05617055 |
| mean anomaly at epoch: | 224.0156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|