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 23705U 95058B 23152.22850874 .00000280 00000-0 16812-3 0 9994
2 23705 71.0203 145.4378 0014079 228.7865 131.2045 14.15233141424891
| Epoch (UTC): | 01 June 2023 05:29:03 |
| Eccentricity: | 0.0014079 |
| inclination: | 71.0203° |
| perigee height: | 831 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 145.4378° |
| argument of perigee: | 228.7865° |
| revolutions per day: | 14.15233141 |
| mean anomaly at epoch: | 131.2045° |
| orbit number at epoch: | 42489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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