View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46672U 26145.58335647 +.00000000 +00000-0 +87770-3 0 00009
2 46672 53.0364 179.0057 0006092 348.5069 257.7264 15.83479712 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0006092 |
| inclination: | 53.0364° |
| perigee height: | 317 km |
| apogee height: | 325 km |
| right ascension of ascending node: | 179.0057° |
| argument of perigee: | 348.5069° |
| revolutions per day: | 15.83479712 |
| mean anomaly at epoch: | 257.7264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|