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 23151.94553944 .00000142 00000-0 64509-4 0 9990
2 12646 81.2254 289.8914 0066455 258.8508 221.7427 14.16028583159273
| Epoch (UTC): | 31 May 2023 22:41:34 |
| Eccentricity: | 0.0066455 |
| inclination: | 81.2254° |
| perigee height: | 791 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 289.8914° |
| argument of perigee: | 258.8508° |
| revolutions per day: | 14.16028583 |
| mean anomaly at epoch: | 221.7427° |
| orbit number at epoch: | 15927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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