View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58133U 26145.44187836 +.00000000 +00000-0 +67185-4 0 00003
2 58133 43.0057 55.7695 0000755 259.5686 100.5081 15.27584324 02
| Epoch (UTC): | 25 May 2026 10:36:18 |
| Eccentricity: | 0.0000755 |
| inclination: | 43.0057° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 55.7695° |
| argument of perigee: | 259.5686° |
| revolutions per day: | 15.27584324 |
| mean anomaly at epoch: | 100.5081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|