View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55915U 26145.31488821 +.00000000 +00000-0 +10188-3 0 00002
2 55915 69.9989 111.3080 0003344 267.3571 92.7205 14.98323636 06
| Epoch (UTC): | 25 May 2026 07:33:26 |
| Eccentricity: | 0.0003344 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 111.3080° |
| argument of perigee: | 267.3571° |
| revolutions per day: | 14.98323636 |
| mean anomaly at epoch: | 92.7205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|