View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61948U 26145.30585485 +.00000000 +00000-0 +16754-2 0 00002
2 61948 53.1574 353.4004 0000841 65.1714 294.9391 15.69788274 05
| Epoch (UTC): | 25 May 2026 07:20:25 |
| Eccentricity: | 0.0000841 |
| inclination: | 53.1574° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 353.4004° |
| argument of perigee: | 65.1714° |
| revolutions per day: | 15.69788274 |
| mean anomaly at epoch: | 294.9391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|