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 24281.44821462 .00001904 00000-0 69077-3 0 9993
2 27601 98.2447 253.0365 0069589 266.7549 204.5450 14.33076888139867
| Epoch (UTC): | 07 October 2024 10:45:25 |
| Eccentricity: | 0.0069589 |
| inclination: | 98.2447° |
| perigee height: | 731 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 253.0365° |
| argument of perigee: | 266.7549° |
| revolutions per day: | 14.33076888 |
| mean anomaly at epoch: | 204.5450° |
| orbit number at epoch: | 13986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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