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 23155.59356681 .00003907 00000-0 20426-3 0 9999
2 20580 28.4707 351.7954 0002129 241.3354 156.4511 15.13177791619556
| Epoch (UTC): | 04 June 2023 14:14:44 |
| Eccentricity: | 0.0002129 |
| inclination: | 28.4707° |
| perigee height: | 525 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 351.7954° |
| argument of perigee: | 241.3354° |
| revolutions per day: | 15.13177791 |
| mean anomaly at epoch: | 156.4511° |
| orbit number at epoch: | 61955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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