View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51789U 26145.63136689 +.00000000 +00000-0 +67792-5 0 00009
2 51789 53.2125 3.7140 0001429 91.3503 268.7653 15.08842710 05
| Epoch (UTC): | 25 May 2026 15:09:10 |
| Eccentricity: | 0.0001429 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 3.7140° |
| argument of perigee: | 91.3503° |
| revolutions per day: | 15.08842710 |
| mean anomaly at epoch: | 268.7653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|