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 41465U 16026B 23333.49247270 .00071863 00000-0 56455-3 0 9997
2 41465 96.9651 202.8673 0004758 2.1704 357.9580 15.71288762425795
| Epoch (UTC): | 29 November 2023 11:49:09 |
| Eccentricity: | 0.0004758 |
| inclination: | 96.9651° |
| perigee height: | 352 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 202.8673° |
| argument of perigee: | 2.1704° |
| revolutions per day: | 15.71288762 |
| mean anomaly at epoch: | 357.9580° |
| orbit number at epoch: | 42579 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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