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 61461U 24140ZT 24356.93827614 .00009153 00000-0 33200-2 0 9997
2 61461 89.1345 337.6113 0026784 27.6266 332.6348 14.33078213 16525
| Epoch (UTC): | 21 December 2024 22:31:07 |
| Eccentricity: | 0.0026784 |
| inclination: | 89.1345° |
| perigee height: | 762 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 337.6113° |
| argument of perigee: | 27.6266° |
| revolutions per day: | 14.33078213 |
| mean anomaly at epoch: | 332.6348° |
| orbit number at epoch: | 1652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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