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 23084.48783417 .00003722 00000-0 52184-3 0 9993
2 27607 64.5554 161.4845 0075700 241.3102 118.0377 14.77006517 90075
| Epoch (UTC): | 25 March 2023 11:42:28 |
| Eccentricity: | 0.0075700 |
| inclination: | 64.5554° |
| perigee height: | 585 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 161.4845° |
| argument of perigee: | 241.3102° |
| revolutions per day: | 14.77006517 |
| mean anomaly at epoch: | 118.0377° |
| orbit number at epoch: | 9007 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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