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 18096U 87049B 23152.42728605 .00000274 00000-0 10132-3 0 9992
2 18096 74.0406 190.3105 0021777 190.8233 169.2455 14.36896437884032
| Epoch (UTC): | 01 June 2023 10:15:17 |
| Eccentricity: | 0.0021777 |
| inclination: | 74.0406° |
| perigee height: | 753 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 190.3105° |
| argument of perigee: | 190.8233° |
| revolutions per day: | 14.36896437 |
| mean anomaly at epoch: | 169.2455° |
| orbit number at epoch: | 88403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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