View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32376U 26044.95432065 +.00000000 +00000-0 +82397-4 0 00007
2 32376 97.8848 230.3359 0001437 83.5720 276.5657 14.82145332 03
| Epoch (UTC): | 13 February 2026 22:54:13 |
| Eccentricity: | 0.0001437 |
| inclination: | 97.8848° |
| perigee height: | 622 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 230.3359° |
| argument of perigee: | 83.5720° |
| revolutions per day: | 14.82145332 |
| mean anomaly at epoch: | 276.5657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|