View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64194U 26145.25935924 +.00000000 +00000-0 +77358-3 0 00007
2 64194 53.1609 95.0911 0001365 85.9835 274.1322 15.31716298 02
| Epoch (UTC): | 25 May 2026 06:13:28 |
| Eccentricity: | 0.0001365 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.0911° |
| argument of perigee: | 85.9835° |
| revolutions per day: | 15.31716298 |
| mean anomaly at epoch: | 274.1322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|