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 11114U 78105D 23333.18222547 .00012506 00000-0 15038-2 0 9997
2 11114 74.0101 246.3901 0003995 352.6901 7.4218 14.83982764389778
| Epoch (UTC): | 29 November 2023 04:22:24 |
| Eccentricity: | 0.0003995 |
| inclination: | 74.0101° |
| perigee height: | 614 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 246.3901° |
| argument of perigee: | 352.6901° |
| revolutions per day: | 14.83982764 |
| mean anomaly at epoch: | 7.4218° |
| orbit number at epoch: | 38977 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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