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 61296U 24140TH 24357.94940468 .00001434 00000-0 62747-3 0 9991
2 61296 89.0987 337.1065 0035034 102.7575 257.7536 14.22931092 16560
| Epoch (UTC): | 22 December 2024 22:47:08 |
| Eccentricity: | 0.0035034 |
| inclination: | 89.0987° |
| perigee height: | 790 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 337.1065° |
| argument of perigee: | 102.7575° |
| revolutions per day: | 14.22931092 |
| mean anomaly at epoch: | 257.7536° |
| orbit number at epoch: | 1656 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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