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 20465U 90010A 23153.47239153 .00002505 00000-0 19623-3 0 9991
2 20465 82.4864 312.9551 0015344 152.4463 207.7578 15.00519271811196
| Epoch (UTC): | 02 June 2023 11:20:14 |
| Eccentricity: | 0.0015344 |
| inclination: | 82.4864° |
| perigee height: | 554 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 312.9551° |
| argument of perigee: | 152.4463° |
| revolutions per day: | 15.00519271 |
| mean anomaly at epoch: | 207.7578° |
| orbit number at epoch: | 81119 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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