View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10962U 26100.14218813 +.00000000 +00000-0 +84615-4 0 00006
2 10962 74.0802 31.8459 0025100 187.7789 172.2982 14.42864620 04
| Epoch (UTC): | 10 April 2026 03:24:45 |
| Eccentricity: | 0.0025100 |
| inclination: | 74.0802° |
| perigee height: | 731 km |
| apogee height: | 767 km |
| right ascension of ascending node: | 31.8459° |
| argument of perigee: | 187.7789° |
| revolutions per day: | 14.42864620 |
| mean anomaly at epoch: | 172.2982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|