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 22184.78401092 .00000176 00000-0 44763-4 0 9997
2 27607 64.5543 251.9274 0079283 291.2803 67.9847 14.76149373 50781
| Epoch (UTC): | 03 July 2022 18:48:58 |
| Eccentricity: | 0.0079283 |
| inclination: | 64.5543° |
| perigee height: | 586 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 251.9274° |
| argument of perigee: | 291.2803° |
| revolutions per day: | 14.76149373 |
| mean anomaly at epoch: | 67.9847° |
| orbit number at epoch: | 5078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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