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 23149.75227555 .00001187 00000-0 18029-3 0 9994
2 27607 64.5547 321.4452 0070724 228.3625 131.1409 14.77254902 99507
| Epoch (UTC): | 29 May 2023 18:03:16 |
| Eccentricity: | 0.0070724 |
| inclination: | 64.5547° |
| perigee height: | 588 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 321.4452° |
| argument of perigee: | 228.3625° |
| revolutions per day: | 14.77254902 |
| mean anomaly at epoch: | 131.1409° |
| orbit number at epoch: | 9950 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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