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 23687U 95055B 22147.50289800 .00000120 00000-0 14398-2 0 9998
2 23687 4.8838 95.8014 7245234 312.7968 5.7822 2.21813615215134
| Epoch (UTC): | 27 May 2022 12:04:10 |
| Eccentricity: | 0.7245234 |
| inclination: | 4.8838° |
| perigee height: | 463 km |
| apogee height: | 36451 km |
| right ascension of ascending node: | 95.8014° |
| argument of perigee: | 312.7968° |
| revolutions per day: | 2.21813615 |
| mean anomaly at epoch: | 5.7822° |
| orbit number at epoch: | 21513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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