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 22148.87744457 .00000543 00000-0 95320-4 0 9995
2 27607 64.5558 1.8067 0077339 298.2545 61.0766 14.76109880 45484
| Epoch (UTC): | 28 May 2022 21:03:31 |
| Eccentricity: | 0.0077339 |
| inclination: | 64.5558° |
| perigee height: | 587 km |
| apogee height: | 696 km |
| right ascension of ascending node: | 1.8067° |
| argument of perigee: | 298.2545° |
| revolutions per day: | 14.76109880 |
| mean anomaly at epoch: | 61.0766° |
| orbit number at epoch: | 4548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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