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 23160.60305400 .00001411 00000-0 83636-3 0 9994
2 00012 32.8953 145.4410 1660270 34.4345 335.3392 11.45618459404560
| Epoch (UTC): | 09 June 2023 14:28:23 |
| Eccentricity: | 0.1660270 |
| inclination: | 32.8953° |
| perigee height: | 554 km |
| apogee height: | 3314 km |
| right ascension of ascending node: | 145.4410° |
| argument of perigee: | 34.4345° |
| revolutions per day: | 11.45618459 |
| mean anomaly at epoch: | 335.3392° |
| orbit number at epoch: | 40456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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