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 51074U 22002CU 24006.49812863 .14378782 25543-5 45989-3 0 9998
2 51074 97.4031 91.8532 0011803 282.1666 77.8312 16.43820293110586
| Epoch (UTC): | 06 January 2024 11:57:18 |
| Eccentricity: | 0.0011803 |
| inclination: | 97.4031° |
| perigee height: | 148 km |
| apogee height: | 163 km |
| right ascension of ascending node: | 91.8532° |
| argument of perigee: | 282.1666° |
| revolutions per day: | 16.43820293 |
| mean anomaly at epoch: | 77.8312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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