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 42941U 17056A 23266.78460746 0.00000000 00000-0 00000-0 0 03
2 42941 62.9767 252.4527 6939492 269.5834 17.5844 2.00617618 05
| Epoch (UTC): | 23 September 2023 18:49:50 |
| Eccentricity: | 0.6939492 |
| inclination: | 62.9767° |
| perigee height: | 1749 km |
| apogee height: | 38605 km |
| right ascension of ascending node: | 252.4527° |
| argument of perigee: | 269.5834° |
| revolutions per day: | 2.00617618 |
| mean anomaly at epoch: | 17.5844° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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