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 23151.85086954 .00001320 00000-0 19827-3 0 9990
2 27607 64.5547 315.0117 0070535 227.9427 131.5662 14.77261391 99818
| Epoch (UTC): | 31 May 2023 20:25:15 |
| Eccentricity: | 0.0070535 |
| inclination: | 64.5547° |
| perigee height: | 588 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 315.0117° |
| argument of perigee: | 227.9427° |
| revolutions per day: | 14.77261391 |
| mean anomaly at epoch: | 131.5662° |
| orbit number at epoch: | 9981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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