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 11681U 80007B 23332.83060576 .00000166 00000-0 15621-3 0 9991
2 11681 82.9300 105.2251 0035087 253.7702 216.2566 13.75571764196196
| Epoch (UTC): | 28 November 2023 19:56:04 |
| Eccentricity: | 0.0035087 |
| inclination: | 82.9300° |
| perigee height: | 954 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 105.2251° |
| argument of perigee: | 253.7702° |
| revolutions per day: | 13.75571764 |
| mean anomaly at epoch: | 216.2566° |
| orbit number at epoch: | 19619 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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