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 12472U 81049A 23336.51586041 .00000050 00000-0 00000-0 0 9990
2 12472 11.0247 322.2392 0002632 256.7021 268.9876 1.00221115113545
| Epoch (UTC): | 02 December 2023 12:22:50 |
| Eccentricity: | 0.0002632 |
| inclination: | 11.0247° |
| perigee height: | 35789 km |
| apogee height: | 35811 km |
| right ascension of ascending node: | 322.2392° |
| argument of perigee: | 256.7021° |
| revolutions per day: | 1.00221115 |
| mean anomaly at epoch: | 268.9876° |
| orbit number at epoch: | 11354 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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