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 23335.12029223 .00002547 00000-0 44242-3 0 9993
2 27939 98.2646 123.6458 0011744 334.3290 136.4778 14.69038711 79043
| Epoch (UTC): | 01 December 2023 02:53:13 |
| Eccentricity: | 0.0011744 |
| inclination: | 98.2646° |
| perigee height: | 656 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 123.6458° |
| argument of perigee: | 334.3290° |
| revolutions per day: | 14.69038711 |
| mean anomaly at epoch: | 136.4778° |
| orbit number at epoch: | 7904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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