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 23332.21406715 .00008132 00000-0 41391-3 0 9998
2 20580 28.4690 255.3124 0002620 358.7440 150.9550 15.15008428646341
| Epoch (UTC): | 28 November 2023 05:08:15 |
| Eccentricity: | 0.0002620 |
| inclination: | 28.4690° |
| perigee height: | 519 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 255.3124° |
| argument of perigee: | 358.7440° |
| revolutions per day: | 15.15008428 |
| mean anomaly at epoch: | 150.9550° |
| orbit number at epoch: | 64634 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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