View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67498U 26145.54051770 +.00000000 +00000-0 +37498-3 0 00008
2 67498 43.0025 240.5330 0002570 259.9164 100.1398 15.27566123 07
| Epoch (UTC): | 25 May 2026 12:58:20 |
| Eccentricity: | 0.0002570 |
| inclination: | 43.0025° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 240.5330° |
| argument of perigee: | 259.9164° |
| revolutions per day: | 15.27566123 |
| mean anomaly at epoch: | 100.1398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|