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 12585U 81065A 23150.04007559 .00007287 00000-0 25795-3 0 9997
2 12585 97.5764 164.9955 0011832 9.1296 351.0157 15.29387006287035
| Epoch (UTC): | 30 May 2023 00:57:42 |
| Eccentricity: | 0.0011832 |
| inclination: | 97.5764° |
| perigee height: | 469 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 164.9955° |
| argument of perigee: | 9.1296° |
| revolutions per day: | 15.29387006 |
| mean anomaly at epoch: | 351.0157° |
| orbit number at epoch: | 28703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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