View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26474U 26065.51613153 +.00000000 +00000-0 +36169-3 0 00008
2 26474 67.9894 49.4334 0038309 39.1527 321.2382 15.09524611 00
| Epoch (UTC): | 06 March 2026 12:23:13 |
| Eccentricity: | 0.0038309 |
| inclination: | 67.9894° |
| perigee height: | 511 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 49.4334° |
| argument of perigee: | 39.1527° |
| revolutions per day: | 15.09524611 |
| mean anomaly at epoch: | 321.2382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|