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 27607U 02058C 23088.88882595 .00002798 00000-0 39731-3 0 9993
2 27607 64.5549 147.9983 0075371 240.4858 118.8715 14.77030561 90512
| Epoch (UTC): | 29 March 2023 21:19:54 |
| Eccentricity: | 0.0075371 |
| inclination: | 64.5549° |
| perigee height: | 586 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 147.9983° |
| argument of perigee: | 240.4858° |
| revolutions per day: | 14.77030561 |
| mean anomaly at epoch: | 118.8715° |
| orbit number at epoch: | 9051 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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