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 23270.67412544 .00002108 00000-0 27854-3 0 9995
2 23342 97.7664 307.8065 0002308 93.4420 266.7057 14.81016517556912
| Epoch (UTC): | 27 September 2023 16:10:44 |
| Eccentricity: | 0.0002308 |
| inclination: | 97.7664° |
| perigee height: | 624 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 307.8065° |
| argument of perigee: | 93.4420° |
| revolutions per day: | 14.81016517 |
| mean anomaly at epoch: | 266.7057° |
| orbit number at epoch: | 55691 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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