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 20303U 89085B 23275.33020858 .00550413 12256-3 13199-2 0 9998
2 20303 35.6242 255.3110 0025423 228.3197 131.5375 15.94861268853222
| Epoch (UTC): | 02 October 2023 07:55:30 |
| Eccentricity: | 0.0025423 |
| inclination: | 35.6242° |
| perigee height: | 272 km |
| apogee height: | 305 km |
| right ascension of ascending node: | 255.3110° |
| argument of perigee: | 228.3197° |
| revolutions per day: | 15.94861268 |
| mean anomaly at epoch: | 131.5375° |
| orbit number at epoch: | 85322 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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