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 61460U 24140ZS 24357.94879320 .00062429 00000-0 94733-2 0 9992
2 61460 89.1583 337.2574 0121481 242.7128 116.1677 14.68873724 14304
| Epoch (UTC): | 22 December 2024 22:46:15 |
| Eccentricity: | 0.0121481 |
| inclination: | 89.1583° |
| perigee height: | 579 km |
| apogee height: | 750 km |
| right ascension of ascending node: | 337.2574° |
| argument of perigee: | 242.7128° |
| revolutions per day: | 14.68873724 |
| mean anomaly at epoch: | 116.1677° |
| orbit number at epoch: | 1430 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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