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 26093U 00004L 23266.22579800 .00003620 00000-0 85138-3 0 9995
2 26093 100.1754 170.2188 0027520 265.9221 93.8824 14.54980483246776
| Epoch (UTC): | 23 September 2023 05:25:08 |
| Eccentricity: | 0.0027520 |
| inclination: | 100.1754° |
| perigee height: | 690 km |
| apogee height: | 729 km |
| right ascension of ascending node: | 170.2188° |
| argument of perigee: | 265.9221° |
| revolutions per day: | 14.54980483 |
| mean anomaly at epoch: | 93.8824° |
| orbit number at epoch: | 24677 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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