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 11U 59001A 23030.23296452 .00001710 00000-0 89555-3 0 9992
2 11 32.8794 61.8015 1463588 254.9226 88.5270 11.86433246730337
| Epoch (UTC): | 30 January 2023 05:35:28 |
| Eccentricity: | 0.1463588 |
| inclination: | 32.8794° |
| perigee height: | 554 km |
| apogee height: | 2930 km |
| right ascension of ascending node: | 61.8015° |
| argument of perigee: | 254.9226° |
| revolutions per day: | 11.86433246 |
| mean anomaly at epoch: | 88.5270° |
| orbit number at epoch: | 73033 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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