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 23091.90577806 -.00000039 00000-0 10000-3 0 9991
2 23439 64.8151 39.0661 0164987 223.5186 135.2619 11.27574020164013
| Epoch (UTC): | 01 April 2023 21:44:19 |
| Eccentricity: | 0.0164987 |
| inclination: | 64.8151° |
| perigee height: | 1884 km |
| apogee height: | 2161 km |
| right ascension of ascending node: | 39.0661° |
| argument of perigee: | 223.5186° |
| revolutions per day: | 11.27574020 |
| mean anomaly at epoch: | 135.2619° |
| orbit number at epoch: | 16401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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