View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65037U 26145.14706546 +.00000000 +00000-0 +29809-3 0 00006
2 65037 53.1626 299.2122 0001467 97.7413 262.3754 15.30206416 09
| Epoch (UTC): | 25 May 2026 03:31:46 |
| Eccentricity: | 0.0001467 |
| inclination: | 53.1626° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 299.2122° |
| argument of perigee: | 97.7413° |
| revolutions per day: | 15.30206416 |
| mean anomaly at epoch: | 262.3754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|