View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00351U 26017.70779900 +.00000000 +00000-0 +13385-2 0 00009
2 00351 66.7406 154.9215 0017782 67.9639 292.3373 14.83041112 06
| Epoch (UTC): | 17 January 2026 16:59:13 |
| Eccentricity: | 0.0017782 |
| inclination: | 66.7406° |
| perigee height: | 607 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 154.9215° |
| argument of perigee: | 67.9639° |
| revolutions per day: | 14.83041112 |
| mean anomaly at epoch: | 292.3373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|