View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 03669U 26133.32196683 +.00000000 +00000-0 +59575-4 0 00005
2 03669 88.4421 148.2324 1706272 318.7055 29.6456 11.30427959 04
| Epoch (UTC): | 13 May 2026 07:43:37 |
| Eccentricity: | 0.1706272 |
| inclination: | 88.4421° |
| perigee height: | 577 km |
| apogee height: | 3439 km |
| right ascension of ascending node: | 148.2324° |
| argument of perigee: | 318.7055° |
| revolutions per day: | 11.30427959 |
| mean anomaly at epoch: | 29.6456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|