View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57640U 26145.05792324 +.00000000 +00000-0 +19977-3 0 00001
2 57640 43.0037 21.4579 0001174 256.1592 103.9130 15.27563335 09
| Epoch (UTC): | 25 May 2026 01:23:24 |
| Eccentricity: | 0.0001174 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.4579° |
| argument of perigee: | 256.1592° |
| revolutions per day: | 15.27563335 |
| mean anomaly at epoch: | 103.9130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|