View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25893U 26071.03580931 +.00000000 +00000-0 +61123-4 0 00002
2 25893 82.9306 169.6941 0029057 172.1101 0.6451 13.76827473 03
| Epoch (UTC): | 12 March 2026 00:51:33 |
| Eccentricity: | 0.0029057 |
| inclination: | 82.9306° |
| perigee height: | 954 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 169.6941° |
| argument of perigee: | 172.1101° |
| revolutions per day: | 13.76827473 |
| mean anomaly at epoch: | 0.6451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|