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 23029.89107128 .00001332 00000-0 80509-3 0 9994
2 00012 32.8948 243.5477 1661101 66.0064 310.5281 11.44926316389578
| Epoch (UTC): | 29 January 2023 21:23:08 |
| Eccentricity: | 0.1661101 |
| inclination: | 32.8948° |
| perigee height: | 556 km |
| apogee height: | 3318 km |
| right ascension of ascending node: | 243.5477° |
| argument of perigee: | 66.0064° |
| revolutions per day: | 11.44926316 |
| mean anomaly at epoch: | 310.5281° |
| orbit number at epoch: | 38957 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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