View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65892U 26073.05660348 +.00000000 +00000-0 +14724-2 0 00003
2 65892 53.1592 351.0179 0001354 80.5347 279.5806 15.30192606 03
| Epoch (UTC): | 14 March 2026 01:21:30 |
| Eccentricity: | 0.0001354 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.0179° |
| argument of perigee: | 80.5347° |
| revolutions per day: | 15.30192606 |
| mean anomaly at epoch: | 279.5806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|