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 12497U 81050B 23333.96866579 .00013710 00000-0 11666-2 0 9991
2 12497 23.9453 178.0822 3418421 307.1609 26.2373 8.47991300 96401
| Epoch (UTC): | 29 November 2023 23:14:52 |
| Eccentricity: | 0.3418421 |
| inclination: | 23.9453° |
| perigee height: | 307 km |
| apogee height: | 7252 km |
| right ascension of ascending node: | 178.0822° |
| argument of perigee: | 307.1609° |
| revolutions per day: | 8.47991300 |
| mean anomaly at epoch: | 26.2373° |
| orbit number at epoch: | 9640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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