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 25612U 66040E 24357.55357521 .00005561 00000-0 59482-2 0 9993
2 25612 100.4665 202.7836 0032748 64.8109 324.8518 13.74035987361053
| Epoch (UTC): | 22 December 2024 13:17:08 |
| Eccentricity: | 0.0032748 |
| inclination: | 100.4665° |
| perigee height: | 961 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 202.7836° |
| argument of perigee: | 64.8109° |
| revolutions per day: | 13.74035987 |
| mean anomaly at epoch: | 324.8518° |
| orbit number at epoch: | 36105 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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