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 12646U 81075B 23150.18965610 .00000115 00000-0 51332-4 0 9992
2 12646 81.2252 291.6214 0066438 263.9450 270.6940 14.16028103159326
| Epoch (UTC): | 30 May 2023 04:33:06 |
| Eccentricity: | 0.0066438 |
| inclination: | 81.2252° |
| perigee height: | 791 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 291.6214° |
| argument of perigee: | 263.9450° |
| revolutions per day: | 14.16028103 |
| mean anomaly at epoch: | 270.6940° |
| orbit number at epoch: | 15932 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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