View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 44612U 17060E 25197.46230431 .00002816 00000-0 29181-3 0 9999
2 44612 97.5920 208.2297 0012579 129.8286 230.4042 14.90735826416800
Epoch (UTC): | 16 July 2025 11:05:43 |
Eccentricity: | 0.0012579 |
inclination: | 97.5920° |
perigee height: | 587 km |
apogee height: | 604 km |
right ascension of ascending node: | 208.2297° |
argument of perigee: | 129.8286° |
revolutions per day: | 14.90735826 |
mean anomaly at epoch: | 230.4042° |
orbit number at epoch: | 41680 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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