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 39135U 13015F 23362.97479334 .13239417 77207-5 55392-3 0 9998
2 39135 64.8206 25.5887 0006113 296.4162 63.6397 16.43253798592339
| Epoch (UTC): | 28 December 2023 23:23:42 |
| Eccentricity: | 0.0006113 |
| inclination: | 64.8206° |
| perigee height: | 153 km |
| apogee height: | 161 km |
| right ascension of ascending node: | 25.5887° |
| argument of perigee: | 296.4162° |
| revolutions per day: | 16.43253798 |
| mean anomaly at epoch: | 63.6397° |
| orbit number at epoch: | 59233 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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