View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39161U 26145.09371502 +.00000000 +00000-0 +17283-3 0 00002
2 39161 97.7307 200.0898 0009803 91.5696 268.6640 14.81317203 00
| Epoch (UTC): | 25 May 2026 02:14:56 |
| Eccentricity: | 0.0009803 |
| inclination: | 97.7307° |
| perigee height: | 618 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 200.0898° |
| argument of perigee: | 91.5696° |
| revolutions per day: | 14.81317203 |
| mean anomaly at epoch: | 268.6640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|