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 40910U 15049M 24092.20923921 .16747303 26701-5 28112-3 0 9997
2 40910 97.4046 122.6776 0010391 231.3491 128.6883 16.47481859473951
| Epoch (UTC): | 01 April 2024 05:01:18 |
| Eccentricity: | 0.0010391 |
| inclination: | 97.4046° |
| perigee height: | 139 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 122.6776° |
| argument of perigee: | 231.3491° |
| revolutions per day: | 16.47481859 |
| mean anomaly at epoch: | 128.6883° |
| orbit number at epoch: | 47395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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