View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39161U 26097.13197625 +.00000000 +00000-0 +24153-3 0 00009
2 39161 97.7358 153.7999 0006928 241.5953 118.4562 14.81191591 05
| Epoch (UTC): | 07 April 2026 03:10:02 |
| Eccentricity: | 0.0006928 |
| inclination: | 97.7358° |
| perigee height: | 621 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 153.7999° |
| argument of perigee: | 241.5953° |
| revolutions per day: | 14.81191591 |
| mean anomaly at epoch: | 118.4562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|