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 25940U 99057A 24282.52311694 .00002126 00000-0 74066-3 0 9996
2 25940 98.8186 264.5939 0005521 29.9178 330.2322 14.36452970308972
| Epoch (UTC): | 08 October 2024 12:33:17 |
| Eccentricity: | 0.0005521 |
| inclination: | 98.8186° |
| perigee height: | 766 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 264.5939° |
| argument of perigee: | 29.9178° |
| revolutions per day: | 14.36452970 |
| mean anomaly at epoch: | 330.2322° |
| orbit number at epoch: | 30897 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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