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 17912U 87038B 23334.17224588 .00000896 00000-0 10489-3 0 9996
2 17912 82.5020 358.2122 0020523 30.9855 329.2566 14.83849340977082
| Epoch (UTC): | 30 November 2023 04:08:02 |
| Eccentricity: | 0.0020523 |
| inclination: | 82.5020° |
| perigee height: | 603 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 358.2122° |
| argument of perigee: | 30.9855° |
| revolutions per day: | 14.83849340 |
| mean anomaly at epoch: | 329.2566° |
| orbit number at epoch: | 97708 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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