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 54816U 21035C 23072.25043904 .02330371 77621-5 12756-2 0 9996
2 54816 41.5077 9.4914 0017840 162.4710 197.7314 16.18206266 13316
| Epoch (UTC): | 13 March 2023 06:00:37 |
| Eccentricity: | 0.0017840 |
| inclination: | 41.5077° |
| perigee height: | 212 km |
| apogee height: | 236 km |
| right ascension of ascending node: | 9.4914° |
| argument of perigee: | 162.4710° |
| revolutions per day: | 16.18206266 |
| mean anomaly at epoch: | 197.7314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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