View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 27609U 02058E 25196.56129509 .00000168 00000-0 40356-4 0 9996
2 27609 64.5562 294.9861 0050519 292.3660 67.2096 14.80877184217830
Epoch (UTC): | 15 July 2025 13:28:15 |
Eccentricity: | 0.0050519 |
inclination: | 64.5562° |
perigee height: | 591 km |
apogee height: | 662 km |
right ascension of ascending node: | 294.9861° |
argument of perigee: | 292.3660° |
revolutions per day: | 14.80877184 |
mean anomaly at epoch: | 67.2096° |
orbit number at epoch: | 21783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|