View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60105U 26145.42126420 +.00000000 +00000-0 +39552-5 0 00003
2 60105 53.1619 40.7665 0001250 96.7608 263.3535 15.30186693 00
| Epoch (UTC): | 25 May 2026 10:06:37 |
| Eccentricity: | 0.0001250 |
| inclination: | 53.1619° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.7665° |
| argument of perigee: | 96.7608° |
| revolutions per day: | 15.30186693 |
| mean anomaly at epoch: | 263.3535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|