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 04159U 69082AB 23150.90355337 .00000044 00000-0 98744-4 0 9994
2 04159 69.9631 1.0782 0117427 265.1138 93.6540 13.72571974685799
| Epoch (UTC): | 30 May 2023 21:41:07 |
| Eccentricity: | 0.0117427 |
| inclination: | 69.9631° |
| perigee height: | 904 km |
| apogee height: | 1077 km |
| right ascension of ascending node: | 1.0782° |
| argument of perigee: | 265.1138° |
| revolutions per day: | 13.72571974 |
| mean anomaly at epoch: | 93.6540° |
| orbit number at epoch: | 68579 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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