View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64362U 26145.38893171 +.00000000 +00000-0 +22351-3 0 00008
2 64362 70.0005 200.9506 0003867 266.0726 93.9991 14.98337981 03
| Epoch (UTC): | 25 May 2026 09:20:03 |
| Eccentricity: | 0.0003867 |
| inclination: | 70.0005° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.9506° |
| argument of perigee: | 266.0726° |
| revolutions per day: | 14.98337981 |
| mean anomaly at epoch: | 93.9991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|