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 61330U 24140UT 24357.92159368 .00005992 00000-0 15555-2 0 9996
2 61330 88.8630 332.4172 0080220 311.7925 47.6444 14.47706679 16029
| Epoch (UTC): | 22 December 2024 22:07:05 |
| Eccentricity: | 0.0080220 |
| inclination: | 88.8630° |
| perigee height: | 676 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 332.4172° |
| argument of perigee: | 311.7925° |
| revolutions per day: | 14.47706679 |
| mean anomaly at epoch: | 47.6444° |
| orbit number at epoch: | 1602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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