View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61574U 26145.37076991 +.00000000 +00000-0 +16998-4 0 00003
2 61574 53.1601 278.2640 0000744 113.9042 246.2054 15.69711410 03
| Epoch (UTC): | 25 May 2026 08:53:54 |
| Eccentricity: | 0.0000744 |
| inclination: | 53.1601° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 278.2640° |
| argument of perigee: | 113.9042° |
| revolutions per day: | 15.69711410 |
| mean anomaly at epoch: | 246.2054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|