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 27060U 01058F 23088.45177441 .00000030 00000-0 10504-3 0 9999
2 27060 82.5399 231.0632 0009251 94.5403 265.6745 12.63018513979394
| Epoch (UTC): | 29 March 2023 10:50:33 |
| Eccentricity: | 0.0009251 |
| inclination: | 82.5399° |
| perigee height: | 1403 km |
| apogee height: | 1418 km |
| right ascension of ascending node: | 231.0632° |
| argument of perigee: | 94.5403° |
| revolutions per day: | 12.63018513 |
| mean anomaly at epoch: | 265.6745° |
| orbit number at epoch: | 97939 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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