View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13066U 26073.33490867 +.00000000 +00000-0 +55632-4 0 00002
2 13066 82.9018 351.3964 0042501 307.1943 174.7964 13.77379906 06
| Epoch (UTC): | 14 March 2026 08:02:16 |
| Eccentricity: | 0.0042501 |
| inclination: | 82.9018° |
| perigee height: | 942 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 351.3964° |
| argument of perigee: | 307.1943° |
| revolutions per day: | 13.77379906 |
| mean anomaly at epoch: | 174.7964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|