View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05104U 26031.87227748 +.00000000 +00000-0 -31510-4 0 00005
2 05104 88.1742 338.0968 0045412 92.2084 322.9141 12.67883350 05
| Epoch (UTC): | 31 January 2026 20:56:04 |
| Eccentricity: | 0.0045412 |
| inclination: | 88.1742° |
| perigee height: | 1355 km |
| apogee height: | 1426 km |
| right ascension of ascending node: | 338.0968° |
| argument of perigee: | 92.2084° |
| revolutions per day: | 12.67883350 |
| mean anomaly at epoch: | 322.9141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|