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 11416U 79057A 23271.89233854 .00000591 00000-0 22689-3 0 9993
2 11416 98.6499 288.2429 0009489 321.1129 38.9372 14.34171624308651
| Epoch (UTC): | 28 September 2023 21:24:58 |
| Eccentricity: | 0.0009489 |
| inclination: | 98.6499° |
| perigee height: | 771 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 288.2429° |
| argument of perigee: | 321.1129° |
| revolutions per day: | 14.34171624 |
| mean anomaly at epoch: | 38.9372° |
| orbit number at epoch: | 30865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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