View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28380U 26145.39667110 +.00000000 +00000-0 +52129-4 0 00008
2 28380 82.9597 91.7122 0038308 317.8717 164.7152 13.76332689 05
| Epoch (UTC): | 25 May 2026 09:31:12 |
| Eccentricity: | 0.0038308 |
| inclination: | 82.9597° |
| perigee height: | 949 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 91.7122° |
| argument of perigee: | 317.8717° |
| revolutions per day: | 13.76332689 |
| mean anomaly at epoch: | 164.7152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|