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 61377U 24140WS 24357.90484344 .00063580 00000-0 76182-2 0 9990
2 61377 89.2361 338.5140 0133796 291.8633 66.8404 14.77552072 16195
| Epoch (UTC): | 22 December 2024 21:42:58 |
| Eccentricity: | 0.0133796 |
| inclination: | 89.2361° |
| perigee height: | 543 km |
| apogee height: | 731 km |
| right ascension of ascending node: | 338.5140° |
| argument of perigee: | 291.8633° |
| revolutions per day: | 14.77552072 |
| mean anomaly at epoch: | 66.8404° |
| orbit number at epoch: | 1619 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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