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 00011U 59001A 24256.66605181 .00003015 00000-0 15912-2 0 9998
2 00011 32.8712 354.1382 1454103 4.5139 356.7116 11.88716622458922
| Epoch (UTC): | 12 September 2024 15:59:06 |
| Eccentricity: | 0.1454103 |
| inclination: | 32.8712° |
| perigee height: | 552 km |
| apogee height: | 2911 km |
| right ascension of ascending node: | 354.1382° |
| argument of perigee: | 4.5139° |
| revolutions per day: | 11.88716622 |
| mean anomaly at epoch: | 356.7116° |
| orbit number at epoch: | 45892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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