View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53004U 26145.18562880 +.00000000 +00000-0 +62707-4 0 00007
2 53004 53.2134 110.7159 0001697 75.0139 285.1040 15.08857566 05
| Epoch (UTC): | 25 May 2026 04:27:18 |
| Eccentricity: | 0.0001697 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.7159° |
| argument of perigee: | 75.0139° |
| revolutions per day: | 15.08857566 |
| mean anomaly at epoch: | 285.1040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|