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 00012U 59001B 23037.82950921 .00002141 00000-0 12859-2 0 9994
2 00012 32.8938 215.7437 1661023 107.7921 271.0272 11.44953343390485
| Epoch (UTC): | 06 February 2023 19:54:29 |
| Eccentricity: | 0.1661023 |
| inclination: | 32.8938° |
| perigee height: | 556 km |
| apogee height: | 3318 km |
| right ascension of ascending node: | 215.7437° |
| argument of perigee: | 107.7921° |
| revolutions per day: | 11.44953343 |
| mean anomaly at epoch: | 271.0272° |
| orbit number at epoch: | 39048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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