View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39161U 26075.10841889 +.00000000 +00000-0 +25109-3 0 00002
2 39161 97.7411 132.5333 0007217 327.3551 32.7215 14.81097641 05
| Epoch (UTC): | 16 March 2026 02:36:07 |
| Eccentricity: | 0.0007217 |
| inclination: | 97.7411° |
| perigee height: | 621 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 132.5333° |
| argument of perigee: | 327.3551° |
| revolutions per day: | 14.81097641 |
| mean anomaly at epoch: | 32.7215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|