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 22182.54834692 .00000158 00000-0 42340-4 0 9994
2 27607 64.5546 258.7689 0079157 291.7156 67.5533 14.76147514 50452
| Epoch (UTC): | 01 July 2022 13:09:37 |
| Eccentricity: | 0.0079157 |
| inclination: | 64.5546° |
| perigee height: | 586 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 258.7689° |
| argument of perigee: | 291.7156° |
| revolutions per day: | 14.76147514 |
| mean anomaly at epoch: | 67.5533° |
| orbit number at epoch: | 5045 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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