View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32785U 26073.88776942 +.00000000 +00000-0 +56187-3 0 00007
2 32785 97.8206 53.4525 0009024 1.3773 358.7478 15.08455682 05
| Epoch (UTC): | 14 March 2026 21:18:23 |
| Eccentricity: | 0.0009024 |
| inclination: | 97.8206° |
| perigee height: | 535 km |
| apogee height: | 547 km |
| right ascension of ascending node: | 53.4525° |
| argument of perigee: | 1.3773° |
| revolutions per day: | 15.08455682 |
| mean anomaly at epoch: | 358.7478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|