View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54741U 26145.56535500 +.00000000 +00000-0 +00000-0 0 00001
2 54741 0.0409 108.4211 0002103 316.7023 288.4485 1.00271797 04
| Epoch (UTC): | 25 May 2026 13:34:06 |
| Eccentricity: | 0.0002103 |
| inclination: | 0.0409° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 108.4211° |
| argument of perigee: | 316.7023° |
| revolutions per day: | 1.00271797 |
| mean anomaly at epoch: | 288.4485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|