View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64261U 26145.58335647 +.00000000 +00000-0 -52977-3 0 00005
2 64261 53.1592 117.2836 0001378 93.9754 156.6625 15.34384986 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001378 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 117.2836° |
| argument of perigee: | 93.9754° |
| revolutions per day: | 15.34384986 |
| mean anomaly at epoch: | 156.6625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|