View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38041U 26145.21433301 +.00000000 +00000-0 +31315-4 0 00001
2 38041 52.0055 88.9280 0000104 120.3658 19.1839 12.62268991 07
| Epoch (UTC): | 25 May 2026 05:08:38 |
| Eccentricity: | 0.0000104 |
| inclination: | 52.0055° |
| perigee height: | 1414 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 88.9280° |
| argument of perigee: | 120.3658° |
| revolutions per day: | 12.62268991 |
| mean anomaly at epoch: | 19.1839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|