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 27939U 03042A 23337.16233894 .00002440 00000-0 42408-3 0 9994
2 27939 98.2646 125.7110 0011620 327.4953 136.3620 14.69050254 79347
| Epoch (UTC): | 03 December 2023 03:53:46 |
| Eccentricity: | 0.0011620 |
| inclination: | 98.2646° |
| perigee height: | 656 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 125.7110° |
| argument of perigee: | 327.4953° |
| revolutions per day: | 14.69050254 |
| mean anomaly at epoch: | 136.3620° |
| orbit number at epoch: | 7934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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