View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46907U 26145.63216866 +.00000000 +00000-0 +24347-3 0 00008
2 46907 36.8961 206.7276 0002674 63.8585 296.2438 15.24365038 06
| Epoch (UTC): | 25 May 2026 15:10:19 |
| Eccentricity: | 0.0002674 |
| inclination: | 36.8961° |
| perigee height: | 491 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 206.7276° |
| argument of perigee: | 63.8585° |
| revolutions per day: | 15.24365038 |
| mean anomaly at epoch: | 296.2438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|