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 410U 61015EK 24276.92048671 .00000373 00000-0 45748-3 0 9990
2 410 66.6916 88.3538 0009106 38.7961 111.5977 13.76424011174918
| Epoch (UTC): | 02 October 2024 22:05:30 |
| Eccentricity: | 0.0009106 |
| inclination: | 66.6916° |
| perigee height: | 970 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 88.3538° |
| argument of perigee: | 38.7961° |
| revolutions per day: | 13.76424011 |
| mean anomaly at epoch: | 111.5977° |
| orbit number at epoch: | 17491 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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