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 23080.38516128 .00003127 00000-0 18515-2 0 9990
2 00012 32.9049 66.6708 1660639 331.8412 20.1306 11.45242631395365
| Epoch (UTC): | 21 March 2023 09:14:37 |
| Eccentricity: | 0.1660639 |
| inclination: | 32.9049° |
| perigee height: | 555 km |
| apogee height: | 3316 km |
| right ascension of ascending node: | 66.6708° |
| argument of perigee: | 331.8412° |
| revolutions per day: | 11.45242631 |
| mean anomaly at epoch: | 20.1306° |
| orbit number at epoch: | 39536 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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