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 61738U 24199D 24358.16126255 .00006689 00000-0 64636-3 0 9997
2 61738 97.3785 220.0097 0008667 89.0598 271.1615 14.93089633 50950
| Epoch (UTC): | 23 December 2024 03:52:13 |
| Eccentricity: | 0.0008667 |
| inclination: | 97.3785° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 220.0097° |
| argument of perigee: | 89.0598° |
| revolutions per day: | 14.93089633 |
| mean anomaly at epoch: | 271.1615° |
| orbit number at epoch: | 5095 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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