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 23152.50071414 .00000149 00000-0 67793-4 0 9995
2 12646 81.2255 289.3445 0066479 257.2419 171.8816 14.16028753159353
| Epoch (UTC): | 01 June 2023 12:01:01 |
| Eccentricity: | 0.0066479 |
| inclination: | 81.2255° |
| perigee height: | 791 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 289.3445° |
| argument of perigee: | 257.2419° |
| revolutions per day: | 14.16028753 |
| mean anomaly at epoch: | 171.8816° |
| orbit number at epoch: | 15935 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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