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 14506U 83113A 23153.51759931 .00000321 00000-0 14448-3 0 9996
2 14506 98.2978 328.7965 0009804 272.9867 155.2075 14.28516436 57134
| Epoch (UTC): | 02 June 2023 12:25:20 |
| Eccentricity: | 0.0009804 |
| inclination: | 98.2978° |
| perigee height: | 789 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 328.7965° |
| argument of perigee: | 272.9867° |
| revolutions per day: | 14.28516436 |
| mean anomaly at epoch: | 155.2075° |
| orbit number at epoch: | 5713 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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