View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25682U 26037.62901258 +.00000000 +00000-0 +14759-3 0 00006
2 25682 97.8601 47.2508 0001641 99.4192 12.2800 14.63781736 07
| Epoch (UTC): | 06 February 2026 15:05:46 |
| Eccentricity: | 0.0001641 |
| inclination: | 97.8601° |
| perigee height: | 680 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 47.2508° |
| argument of perigee: | 99.4192° |
| revolutions per day: | 14.63781736 |
| mean anomaly at epoch: | 12.2800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|