View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59839U 26145.45965453 +.00000000 +00000-0 +11996-4 0 00006
2 59839 43.0004 201.1559 0001164 273.9425 86.1294 15.27580189 00
| Epoch (UTC): | 25 May 2026 11:01:54 |
| Eccentricity: | 0.0001164 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 201.1559° |
| argument of perigee: | 273.9425° |
| revolutions per day: | 15.27580189 |
| mean anomaly at epoch: | 86.1294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|