View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61943U 26145.59977331 +.00000000 +00000-0 +14609-2 0 00000
2 61943 53.1565 352.4069 0001015 113.0622 247.0503 15.69772526 02
| Epoch (UTC): | 25 May 2026 14:23:40 |
| Eccentricity: | 0.0001015 |
| inclination: | 53.1565° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 352.4069° |
| argument of perigee: | 113.0622° |
| revolutions per day: | 15.69772526 |
| mean anomaly at epoch: | 247.0503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|