View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67201U 26145.54913396 +.00000000 +00000-0 +32978-3 0 00009
2 67201 70.0021 340.8222 0002202 267.0329 93.0578 14.98336948 01
| Epoch (UTC): | 25 May 2026 13:10:45 |
| Eccentricity: | 0.0002202 |
| inclination: | 70.0021° |
| perigee height: | 571 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.8222° |
| argument of perigee: | 267.0329° |
| revolutions per day: | 14.98336948 |
| mean anomaly at epoch: | 93.0578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|