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 23343U 94074B 23152.16746458 .00000495 00000-0 76548-4 0 9995
2 23343 97.8407 201.6104 0005343 268.8325 157.7755 14.77450350537856
| Epoch (UTC): | 01 June 2023 04:01:08 |
| Eccentricity: | 0.0005343 |
| inclination: | 97.8407° |
| perigee height: | 633 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 201.6104° |
| argument of perigee: | 268.8325° |
| revolutions per day: | 14.77450350 |
| mean anomaly at epoch: | 157.7755° |
| orbit number at epoch: | 53785 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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