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 23152.06462645 -.00000008 00000-0 -24078-4 0 9995
2 23604 82.9028 338.5974 0023072 306.3059 53.5966 13.74353400399741
| Epoch (UTC): | 01 June 2023 01:33:03 |
| Eccentricity: | 0.0023072 |
| inclination: | 82.9028° |
| perigee height: | 967 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 338.5974° |
| argument of perigee: | 306.3059° |
| revolutions per day: | 13.74353400 |
| mean anomaly at epoch: | 53.5966° |
| orbit number at epoch: | 39974 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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