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 27136U 01049CG 23335.61647794 .00008918 00000-0 81098-3 0 9998
2 27136 98.0173 15.6530 0036427 197.1680 282.7580 14.94954133205386
| Epoch (UTC): | 01 December 2023 14:47:43 |
| Eccentricity: | 0.0036427 |
| inclination: | 98.0173° |
| perigee height: | 557 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 15.6530° |
| argument of perigee: | 197.1680° |
| revolutions per day: | 14.94954133 |
| mean anomaly at epoch: | 282.7580° |
| orbit number at epoch: | 20538 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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