View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18959U 26065.39099428 +.00000000 +00000-0 +78101-4 0 00009
2 18959 82.5398 172.7394 0017470 68.9451 291.3631 14.85671694 00
| Epoch (UTC): | 06 March 2026 09:23:01 |
| Eccentricity: | 0.0017470 |
| inclination: | 82.5398° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 172.7394° |
| argument of perigee: | 68.9451° |
| revolutions per day: | 14.85671694 |
| mean anomaly at epoch: | 291.3631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|