View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65874U 26145.58335647 +.00000000 +00000-0 -44750-3 0 00006
2 65874 53.1601 297.0385 0001197 86.1776 71.7276 15.33557590 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001197 |
| inclination: | 53.1601° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 297.0385° |
| argument of perigee: | 86.1776° |
| revolutions per day: | 15.33557590 |
| mean anomaly at epoch: | 71.7276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|