View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59014U 26145.52892991 +.00000000 +00000-0 -53724-4 0 00001
2 59014 53.1621 81.5004 0001306 95.0946 265.0204 15.30178358 00
| Epoch (UTC): | 25 May 2026 12:41:39 |
| Eccentricity: | 0.0001306 |
| inclination: | 53.1621° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.5004° |
| argument of perigee: | 95.0946° |
| revolutions per day: | 15.30178358 |
| mean anomaly at epoch: | 265.0204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|