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 12976U 81116B 24357.53408937 -.00000011 00000-0 38248-4 0 9994
2 12976 73.9833 19.2412 0094891 322.7013 153.1864 12.28390285931234
| Epoch (UTC): | 22 December 2024 12:49:05 |
| Eccentricity: | 0.0094891 |
| inclination: | 73.9833° |
| perigee height: | 1481 km |
| apogee height: | 1631 km |
| right ascension of ascending node: | 19.2412° |
| argument of perigee: | 322.7013° |
| revolutions per day: | 12.28390285 |
| mean anomaly at epoch: | 153.1864° |
| orbit number at epoch: | 93123 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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