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 27601U 02056E 24276.76011590 .00002001 00000-0 72569-3 0 9994
2 27601 98.2440 248.5723 0069625 281.0212 138.1624 14.33060884139195
| Epoch (UTC): | 02 October 2024 18:14:34 |
| Eccentricity: | 0.0069625 |
| inclination: | 98.2440° |
| perigee height: | 731 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 248.5723° |
| argument of perigee: | 281.0212° |
| revolutions per day: | 14.33060884 |
| mean anomaly at epoch: | 138.1624° |
| orbit number at epoch: | 13919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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