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 23132U 94035A 23270.15882716 -.00000324 00000-0 00000-0 0 9994
2 23132 11.9474 11.3818 0004584 166.0983 21.2811 1.00313613121732
| Epoch (UTC): | 27 September 2023 03:48:42 |
| Eccentricity: | 0.0004584 |
| inclination: | 11.9474° |
| perigee height: | 35755 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 11.3818° |
| argument of perigee: | 166.0983° |
| revolutions per day: | 1.00313613 |
| mean anomaly at epoch: | 21.2811° |
| orbit number at epoch: | 12173 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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