View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61546U 26145.58335647 +.00000000 +00000-0 +14195-2 0 00006
2 61546 53.1602 16.8589 0001076 98.2777 81.3843 15.34364660 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001076 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 16.8589° |
| argument of perigee: | 98.2777° |
| revolutions per day: | 15.34364660 |
| mean anomaly at epoch: | 81.3843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|