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 27058U 01058D 23274.00457079 .00000039 00000-0 15766-3 0 9996
2 27058 82.5302 117.1075 0003983 80.7482 279.4059 12.62048140 2374
| Epoch (UTC): | 01 October 2023 00:06:34 |
| Eccentricity: | 0.0003983 |
| inclination: | 82.5302° |
| perigee height: | 1411 km |
| apogee height: | 1417 km |
| right ascension of ascending node: | 117.1075° |
| argument of perigee: | 80.7482° |
| revolutions per day: | 12.62048140 |
| mean anomaly at epoch: | 279.4059° |
| orbit number at epoch: | 237 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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