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 23439U 94085A 23151.41682534 -.00000049 00000-0 -18997-3 0 9994
2 23439 64.8173 302.8092 0162739 213.1575 145.9065 11.27574235170722
| Epoch (UTC): | 31 May 2023 10:00:13 |
| Eccentricity: | 0.0162739 |
| inclination: | 64.8173° |
| perigee height: | 1885 km |
| apogee height: | 2159 km |
| right ascension of ascending node: | 302.8092° |
| argument of perigee: | 213.1575° |
| revolutions per day: | 11.27574235 |
| mean anomaly at epoch: | 145.9065° |
| orbit number at epoch: | 17072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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