View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60440U 26145.49774435 +.00000000 +00000-0 -17190-4 0 00001
2 60440 53.1593 219.3154 0000960 88.4720 271.6392 15.34381997 01
| Epoch (UTC): | 25 May 2026 11:56:45 |
| Eccentricity: | 0.0000960 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.3154° |
| argument of perigee: | 88.4720° |
| revolutions per day: | 15.34381997 |
| mean anomaly at epoch: | 271.6392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|