View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62323U 26145.63601203 +.00000000 +00000-0 +25043-4 0 00006
2 62323 86.5000 350.8495 0001498 82.2399 277.8905 13.24408992 06
| Epoch (UTC): | 25 May 2026 15:15:51 |
| Eccentricity: | 0.0001498 |
| inclination: | 86.5000° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 350.8495° |
| argument of perigee: | 82.2399° |
| revolutions per day: | 13.24408992 |
| mean anomaly at epoch: | 277.8905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|