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 41465U 16026B 23089.57571307 .00035345 00000-0 55154-3 0 9995
2 41465 97.0112 322.4319 0009161 155.6657 290.9724 15.53705757387745
| Epoch (UTC): | 30 March 2023 13:49:01 |
| Eccentricity: | 0.0009161 |
| inclination: | 97.0112° |
| perigee height: | 400 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 322.4319° |
| argument of perigee: | 155.6657° |
| revolutions per day: | 15.53705757 |
| mean anomaly at epoch: | 290.9724° |
| orbit number at epoch: | 38774 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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