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 24725U 97006A 23088.55688140 .00000026 00000-0 89556-4 0 9995
2 24725 82.6064 305.0347 0008211 262.4272 97.5886 12.60684041201713
| Epoch (UTC): | 29 March 2023 13:21:54 |
| Eccentricity: | 0.0008211 |
| inclination: | 82.6064° |
| perigee height: | 1414 km |
| apogee height: | 1426 km |
| right ascension of ascending node: | 305.0347° |
| argument of perigee: | 262.4272° |
| revolutions per day: | 12.60684041 |
| mean anomaly at epoch: | 97.5886° |
| orbit number at epoch: | 20171 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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