View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00205U 26087.98569970 +.00000000 +00000-0 +18080-4 0 00007
2 00205 32.4395 199.1379 0101708 84.6401 276.5814 13.62569389 09
| Epoch (UTC): | 28 March 2026 23:39:24 |
| Eccentricity: | 0.0101708 |
| inclination: | 32.4395° |
| perigee height: | 951 km |
| apogee height: | 1102 km |
| right ascension of ascending node: | 199.1379° |
| argument of perigee: | 84.6401° |
| revolutions per day: | 13.62569389 |
| mean anomaly at epoch: | 276.5814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|