View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13590U 26088.18542417 +.00000000 +00000-0 -20772-4 0 00000
2 13590 82.6114 153.4387 0007236 119.4843 294.3592 12.42685625 06
| Epoch (UTC): | 29 March 2026 04:27:00 |
| Eccentricity: | 0.0007236 |
| inclination: | 82.6114° |
| perigee height: | 1490 km |
| apogee height: | 1501 km |
| right ascension of ascending node: | 153.4387° |
| argument of perigee: | 119.4843° |
| revolutions per day: | 12.42685625 |
| mean anomaly at epoch: | 294.3592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|