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 is defined by the following mean orbital elements,
1 45873U 20046A 23070.76218785 0.00100000 00000-0 40177-2 0 00
2 45873 54.4328 15.4161 0001973 94.5816 265.4183 15.24447129 04
| Epoch (UTC): | 11 March 2023 18:17:33 |
| Eccentricity: | 0.0001973 |
| inclination: | 54.4328° |
| perigee height: | 491 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 15.4161° |
| argument of perigee: | 94.5816° |
| revolutions per day: | 15.24447129 |
| mean anomaly at epoch: | 265.4183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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