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 23150.44123503 -.00000040 00000-0 68990-4 0 9991
2 23439 64.8173 304.3871 0162755 213.3278 145.7314 11.27574209170326
| Epoch (UTC): | 30 May 2023 10:35:22 |
| Eccentricity: | 0.0162755 |
| inclination: | 64.8173° |
| perigee height: | 1885 km |
| apogee height: | 2159 km |
| right ascension of ascending node: | 304.3871° |
| argument of perigee: | 213.3278° |
| revolutions per day: | 11.27574209 |
| mean anomaly at epoch: | 145.7314° |
| orbit number at epoch: | 17032 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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