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 15618U 85023B 24357.88715968 .00000000 00000-0 10681-3 0 9991
2 15618 74.0525 171.3781 0012427 149.9511 319.9134 12.45346778807484
| Epoch (UTC): | 22 December 2024 21:17:30 |
| Eccentricity: | 0.0012427 |
| inclination: | 74.0525° |
| perigee height: | 1474 km |
| apogee height: | 1494 km |
| right ascension of ascending node: | 171.3781° |
| argument of perigee: | 149.9511° |
| revolutions per day: | 12.45346778 |
| mean anomaly at epoch: | 319.9134° |
| orbit number at epoch: | 80748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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