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 23604U 95032B 23152.50144058 -.00000011 00000-0 -27252-4 0 9990
2 23604 82.9027 338.2723 0023050 305.0176 54.8816 13.74353352399576
| Epoch (UTC): | 01 June 2023 12:02:04 |
| Eccentricity: | 0.0023050 |
| inclination: | 82.9027° |
| perigee height: | 967 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 338.2723° |
| argument of perigee: | 305.0176° |
| revolutions per day: | 13.74353352 |
| mean anomaly at epoch: | 54.8816° |
| orbit number at epoch: | 39957 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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