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 41789U 16059G 23083.47418260 .00002124 00000-0 40108-3 0 9993
2 41789 97.8793 123.5379 0027118 352.7455 7.3359 14.65206850346865
| Epoch (UTC): | 24 March 2023 11:22:49 |
| Eccentricity: | 0.0027118 |
| inclination: | 97.8793° |
| perigee height: | 657 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 123.5379° |
| argument of perigee: | 352.7455° |
| revolutions per day: | 14.65206850 |
| mean anomaly at epoch: | 7.3359° |
| orbit number at epoch: | 34686 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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