View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 35499U 26053.65097169 +.00000000 +00000-0 +19526-3 0 00008
2 35499 82.4941 150.9260 0015946 33.2469 326.9609 12.43006054 05
| Epoch (UTC): | 22 February 2026 15:37:23 |
| Eccentricity: | 0.0015946 |
| inclination: | 82.4941° |
| perigee height: | 1481 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 150.9260° |
| argument of perigee: | 33.2469° |
| revolutions per day: | 12.43006054 |
| mean anomaly at epoch: | 326.9609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|