View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64196U 26145.14285970 +.00000000 +00000-0 +55836-3 0 00003
2 64196 53.1592 95.7862 0001147 87.8420 272.2713 15.31715105 05
| Epoch (UTC): | 25 May 2026 03:25:43 |
| Eccentricity: | 0.0001147 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 95.7862° |
| argument of perigee: | 87.8420° |
| revolutions per day: | 15.31715105 |
| mean anomaly at epoch: | 272.2713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|