View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65701U 26144.98496473 +.00000000 +00000-0 -28187-3 0 00009
2 65701 53.1591 351.3592 0001076 80.4765 279.6358 15.30187226 02
| Epoch (UTC): | 24 May 2026 23:38:20 |
| Eccentricity: | 0.0001076 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.3592° |
| argument of perigee: | 80.4765° |
| revolutions per day: | 15.30187226 |
| mean anomaly at epoch: | 279.6358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|