View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62834U 26145.56478407 +.00000000 +00000-0 +11553-2 0 00002
2 62834 43.0034 202.3859 0001584 267.2798 92.7889 15.70862661 02
| Epoch (UTC): | 25 May 2026 13:33:17 |
| Eccentricity: | 0.0001584 |
| inclination: | 43.0034° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 202.3859° |
| argument of perigee: | 267.2798° |
| revolutions per day: | 15.70862661 |
| mean anomaly at epoch: | 92.7889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|