View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32376U 26017.95013816 +.00000000 +00000-0 +61910-4 0 00004
2 32376 97.8817 203.7309 0001299 85.5409 274.5953 14.82158627 08
| Epoch (UTC): | 17 January 2026 22:48:11 |
| Eccentricity: | 0.0001299 |
| inclination: | 97.8817° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 203.7309° |
| argument of perigee: | 85.5409° |
| revolutions per day: | 14.82158627 |
| mean anomaly at epoch: | 274.5953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|