View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05104U 26103.91133182 +.00000000 +00000-0 +72277-4 0 00002
2 05104 88.1675 326.6271 0042206 273.6900 96.3067 12.67884970 08
| Epoch (UTC): | 13 April 2026 21:52:19 |
| Eccentricity: | 0.0042206 |
| inclination: | 88.1675° |
| perigee height: | 1358 km |
| apogee height: | 1423 km |
| right ascension of ascending node: | 326.6271° |
| argument of perigee: | 273.6900° |
| revolutions per day: | 12.67884970 |
| mean anomaly at epoch: | 96.3067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|