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 23088U 94023B 24260.95285252 .00000277 00000-0 16823-3 0 9990
2 23088 70.9980 122.1928 0002596 357.0657 3.0449 14.14879921569888
| Epoch (UTC): | 16 September 2024 22:52:06 |
| Eccentricity: | 0.0002596 |
| inclination: | 70.9980° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 122.1928° |
| argument of perigee: | 357.0657° |
| revolutions per day: | 14.14879921 |
| mean anomaly at epoch: | 3.0449° |
| orbit number at epoch: | 56988 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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