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 46286U 20061Q 24277.17998051 .00118678 00000-0 14864-2 0 9993
2 46286 97.3399 353.0932 0003902 194.0238 166.0911 15.59370801226704
| Epoch (UTC): | 03 October 2024 04:19:10 |
| Eccentricity: | 0.0003902 |
| inclination: | 97.3399° |
| perigee height: | 387 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 353.0932° |
| argument of perigee: | 194.0238° |
| revolutions per day: | 15.59370801 |
| mean anomaly at epoch: | 166.0911° |
| orbit number at epoch: | 22670 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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