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 38384U 65027CM 24277.22947195 .00001169 00000-0 39598-2 0 9990
2 38384 90.2590 2.3928 0018847 190.6033 169.4693 12.98160773583623
| Epoch (UTC): | 03 October 2024 05:30:26 |
| Eccentricity: | 0.0018847 |
| inclination: | 90.2590° |
| perigee height: | 1255 km |
| apogee height: | 1284 km |
| right ascension of ascending node: | 2.3928° |
| argument of perigee: | 190.6033° |
| revolutions per day: | 12.98160773 |
| mean anomaly at epoch: | 169.4693° |
| orbit number at epoch: | 58362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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