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 57400U 23101B 24358.16895723 .00012323 00000-0 54858-3 0 9990
2 57400 97.3373 50.1327 0005356 248.0480 112.0187 15.21591979 79110
| Epoch (UTC): | 23 December 2024 04:03:17 |
| Eccentricity: | 0.0005356 |
| inclination: | 97.3373° |
| perigee height: | 497 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 50.1327° |
| argument of perigee: | 248.0480° |
| revolutions per day: | 15.21591979 |
| mean anomaly at epoch: | 112.0187° |
| orbit number at epoch: | 7911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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