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 25407U 98045B 24283.86141839 .00000251 00000-0 15099-3 0 9998
2 25407 71.0115 186.2553 0005274 92.9762 267.1965 14.16053006354079
| Epoch (UTC): | 09 October 2024 20:40:26 |
| Eccentricity: | 0.0005274 |
| inclination: | 71.0115° |
| perigee height: | 835 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 186.2553° |
| argument of perigee: | 92.9762° |
| revolutions per day: | 14.16053006 |
| mean anomaly at epoch: | 267.1965° |
| orbit number at epoch: | 35407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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