View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 06173U 26106.77258272 +.00000000 +00000-0 +88175-4 0 00008
2 06173 90.0217 208.5862 0047447 244.6667 278.3421 14.52591043 01
| Epoch (UTC): | 16 April 2026 18:32:31 |
| Eccentricity: | 0.0047447 |
| inclination: | 90.0217° |
| perigee height: | 684 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 208.5862° |
| argument of perigee: | 244.6667° |
| revolutions per day: | 14.52591043 |
| mean anomaly at epoch: | 278.3421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|