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 23132U 94035A 23079.88452022 -.00000161 00000-0 00000-0 0 9993
2 23132 11.8769 12.4643 0001520 38.9699 161.7654 1.00394244119825
| Epoch (UTC): | 20 March 2023 21:13:42 |
| Eccentricity: | 0.0001520 |
| inclination: | 11.8769° |
| perigee height: | 35745 km |
| apogee height: | 35758 km |
| right ascension of ascending node: | 12.4643° |
| argument of perigee: | 38.9699° |
| revolutions per day: | 1.00394244 |
| mean anomaly at epoch: | 161.7654° |
| orbit number at epoch: | 11982 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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