View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25489U 26146.26359705 +.00000000 +00000-0 +11589-3 0 00004
2 25489 84.9828 348.1772 0010468 127.5967 232.6188 14.51828005 01
| Epoch (UTC): | 26 May 2026 06:19:34 |
| Eccentricity: | 0.0010468 |
| inclination: | 84.9828° |
| perigee height: | 712 km |
| apogee height: | 727 km |
| right ascension of ascending node: | 348.1772° |
| argument of perigee: | 127.5967° |
| revolutions per day: | 14.51828005 |
| mean anomaly at epoch: | 232.6188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|