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 00045U 60007A 25080.50199939 .00000720 00000-0 20445-3 0 9999
2 00045 66.6923 117.0977 0244286 130.7313 231.5285 14.35433940315066
| Epoch (UTC): | 21 March 2025 12:02:52 |
| Eccentricity: | 0.0244286 |
| inclination: | 66.6923° |
| perigee height: | 599 km |
| apogee height: | 948 km |
| right ascension of ascending node: | 117.0977° |
| argument of perigee: | 130.7313° |
| revolutions per day: | 14.35433940 |
| mean anomaly at epoch: | 231.5285° |
| orbit number at epoch: | 31506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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