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 22175.21075924 .00011993 00000-0 28601-3 0 9995
2 41465 97.0560 51.3281 0011535 104.4057 48.5064 15.41630482344579
| Epoch (UTC): | 24 June 2022 05:03:29 |
| Eccentricity: | 0.0011535 |
| inclination: | 97.0560° |
| perigee height: | 433 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 51.3281° |
| argument of perigee: | 104.4057° |
| revolutions per day: | 15.41630482 |
| mean anomaly at epoch: | 48.5064° |
| orbit number at epoch: | 34457 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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