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 26715U 01009A 23267.54421970 .00000011 00000-0 00000-0 0 9995
2 26715 10.4673 25.1424 0002385 181.2307 228.4583 1.00274355 22960
| Epoch (UTC): | 24 September 2023 13:03:40 |
| Eccentricity: | 0.0002385 |
| inclination: | 10.4673° |
| perigee height: | 35775 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 25.1424° |
| argument of perigee: | 181.2307° |
| revolutions per day: | 1.00274355 |
| mean anomaly at epoch: | 228.4583° |
| orbit number at epoch: | 2296 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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