View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00020U 26157.69051519 +.00000000 +00000-0 +16946-3 0 00001
2 00020 33.3464 304.7342 1637818 357.3002 1.9567 11.61963301 03
| Epoch (UTC): | 06 June 2026 16:34:20 |
| Eccentricity: | 0.1637818 |
| inclination: | 33.3464° |
| perigee height: | 507 km |
| apogee height: | 3204 km |
| right ascension of ascending node: | 304.7342° |
| argument of perigee: | 357.3002° |
| revolutions per day: | 11.61963301 |
| mean anomaly at epoch: | 1.9567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|