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 23342U 94074A 23152.83074887 .00001227 00000-0 16627-3 0 9993
2 23342 97.7761 193.5800 0002314 102.2601 257.8871 14.80670868539206
| Epoch (UTC): | 01 June 2023 19:56:16 |
| Eccentricity: | 0.0002314 |
| inclination: | 97.7761° |
| perigee height: | 625 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 193.5800° |
| argument of perigee: | 102.2601° |
| revolutions per day: | 14.80670868 |
| mean anomaly at epoch: | 257.8871° |
| orbit number at epoch: | 53920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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