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 00446U 62060A 23083.10574573 -.00000097 00000-0 58217-4 0 9990
2 00446 50.1415 304.0560 0070394 109.7617 61.9010 13.35297902945910
| Epoch (UTC): | 24 March 2023 02:32:16 |
| Eccentricity: | 0.0070394 |
| inclination: | 50.1415° |
| perigee height: | 1074 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 304.0560° |
| argument of perigee: | 109.7617° |
| revolutions per day: | 13.35297902 |
| mean anomaly at epoch: | 61.9010° |
| orbit number at epoch: | 94591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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