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 23862U 96029D 23087.75087109 0.00002786 00000-0 73121-3 0 07
2 23862 63.3382 14.4987 0786393 33.3007 326.6993 13.41550909 08
| Epoch (UTC): | 28 March 2023 18:01:15 |
| Eccentricity: | 0.0786393 |
| inclination: | 63.3382° |
| perigee height: | 515 km |
| apogee height: | 1692 km |
| right ascension of ascending node: | 14.4987° |
| argument of perigee: | 33.3007° |
| revolutions per day: | 13.41550909 |
| mean anomaly at epoch: | 326.6993° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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