View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57454U 26145.59860699 +.00000000 +00000-0 +26300-3 0 00002
2 57454 34.9945 221.4303 0016119 269.9785 89.9081 15.18065716 05
| Epoch (UTC): | 25 May 2026 14:21:59 |
| Eccentricity: | 0.0016119 |
| inclination: | 34.9945° |
| perigee height: | 501 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 221.4303° |
| argument of perigee: | 269.9785° |
| revolutions per day: | 15.18065716 |
| mean anomaly at epoch: | 89.9081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|