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 23753U 95072C 24281.41788322 .00000489 00000-0 22035-3 0 9991
2 23753 98.7876 341.3894 0004708 90.4316 269.7404 14.26819229497816
| Epoch (UTC): | 07 October 2024 10:01:45 |
| Eccentricity: | 0.0004708 |
| inclination: | 98.7876° |
| perigee height: | 799 km |
| apogee height: | 806 km |
| right ascension of ascending node: | 341.3894° |
| argument of perigee: | 90.4316° |
| revolutions per day: | 14.26819229 |
| mean anomaly at epoch: | 269.7404° |
| orbit number at epoch: | 49781 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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