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 20580U 90037B 23266.58288934 .00006051 00000-0 31345-3 0 9991
2 20580 28.4706 332.8927 0002306 15.5401 129.6065 15.14119072636381
| Epoch (UTC): | 23 September 2023 13:59:21 |
| Eccentricity: | 0.0002306 |
| inclination: | 28.4706° |
| perigee height: | 522 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 332.8927° |
| argument of perigee: | 15.5401° |
| revolutions per day: | 15.14119072 |
| mean anomaly at epoch: | 129.6065° |
| orbit number at epoch: | 63638 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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