View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58534U 26145.46893137 +.00000000 +00000-0 +95443-6 0 00008
2 58534 53.1610 55.9796 0001154 93.7749 266.3384 15.31704726 02
| Epoch (UTC): | 25 May 2026 11:15:15 |
| Eccentricity: | 0.0001154 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 55.9796° |
| argument of perigee: | 93.7749° |
| revolutions per day: | 15.31704726 |
| mean anomaly at epoch: | 266.3384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|