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 00877U 64053B 22147.87800055 .00000183 00000-0 62436-4 0 9996
2 00877 65.0792 55.6303 0052325 131.2144 229.3484 14.59533385 65018
| Epoch (UTC): | 27 May 2022 21:04:19 |
| Eccentricity: | 0.0052325 |
| inclination: | 65.0792° |
| perigee height: | 657 km |
| apogee height: | 731 km |
| right ascension of ascending node: | 55.6303° |
| argument of perigee: | 131.2144° |
| revolutions per day: | 14.59533385 |
| mean anomaly at epoch: | 229.3484° |
| orbit number at epoch: | 6501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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