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 61075U 24140MR 24357.45715489 .00008128 00000-0 14030-2 0 9993
2 61075 89.0757 335.8802 0154386 320.1855 38.8109 14.60788665 17791
| Epoch (UTC): | 22 December 2024 10:58:18 |
| Eccentricity: | 0.0154386 |
| inclination: | 89.0757° |
| perigee height: | 581 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 335.8802° |
| argument of perigee: | 320.1855° |
| revolutions per day: | 14.60788665 |
| mean anomaly at epoch: | 38.8109° |
| orbit number at epoch: | 1779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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