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 24258.51019000 .00006570 00000-0 10873-2 0 9995
2 27939 98.3016 56.2121 0012517 135.1626 316.7281 14.70598022121400
| Epoch (UTC): | 14 September 2024 12:14:40 |
| Eccentricity: | 0.0012517 |
| inclination: | 98.3016° |
| perigee height: | 650 km |
| apogee height: | 668 km |
| right ascension of ascending node: | 56.2121° |
| argument of perigee: | 135.1626° |
| revolutions per day: | 14.70598022 |
| mean anomaly at epoch: | 316.7281° |
| orbit number at epoch: | 12140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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