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 23150.70002876 .00001214 00000-0 18400-3 0 9992
2 27607 64.5547 318.5397 0070650 228.1748 131.3309 14.77257614 99643
| Epoch (UTC): | 30 May 2023 16:48:02 |
| Eccentricity: | 0.0070650 |
| inclination: | 64.5547° |
| perigee height: | 588 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 318.5397° |
| argument of perigee: | 228.1748° |
| revolutions per day: | 14.77257614 |
| mean anomaly at epoch: | 131.3309° |
| orbit number at epoch: | 9964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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