View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53014U 26145.28222448 +.00000000 +00000-0 +97926-5 0 00004
2 53014 53.2133 100.2815 0001316 79.5605 280.5535 15.08845464 05
| Epoch (UTC): | 25 May 2026 06:46:24 |
| Eccentricity: | 0.0001316 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.2815° |
| argument of perigee: | 79.5605° |
| revolutions per day: | 15.08845464 |
| mean anomaly at epoch: | 280.5535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|