View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53002U 26145.19298345 +.00000000 +00000-0 +56250-4 0 00004
2 53002 53.2139 110.6832 0001532 84.6391 275.4776 15.08845462 09
| Epoch (UTC): | 25 May 2026 04:37:53 |
| Eccentricity: | 0.0001532 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.6832° |
| argument of perigee: | 84.6391° |
| revolutions per day: | 15.08845462 |
| mean anomaly at epoch: | 275.4776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|