View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 32376U 26040.83617553 +.00000000 +00000-0 +89905-4 0 00009
2 32376 97.8844 226.2782 0001503 81.8209 278.3174 14.82158669 01
| Epoch (UTC): | 09 February 2026 20:04:05 |
| Eccentricity: | 0.0001503 |
| inclination: | 97.8844° |
| perigee height: | 621 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 226.2782° |
| argument of perigee: | 81.8209° |
| revolutions per day: | 14.82158669 |
| mean anomaly at epoch: | 278.3174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|