View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61845U 26145.49362757 +.00000000 +00000-0 +71228-4 0 00002
2 61845 42.9995 153.0101 0000495 258.0660 102.0137 15.27569176 03
| Epoch (UTC): | 25 May 2026 11:50:49 |
| Eccentricity: | 0.0000495 |
| inclination: | 42.9995° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 153.0101° |
| argument of perigee: | 258.0660° |
| revolutions per day: | 15.27569176 |
| mean anomaly at epoch: | 102.0137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|