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 29092U 06015A 23151.93917873 .00000879 00000-0 11158-3 0 9996
2 29092 97.8390 179.4436 0001521 92.4485 267.6904 14.84136492924613
| Epoch (UTC): | 31 May 2023 22:32:25 |
| Eccentricity: | 0.0001521 |
| inclination: | 97.8390° |
| perigee height: | 615 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 179.4436° |
| argument of perigee: | 92.4485° |
| revolutions per day: | 14.84136492 |
| mean anomaly at epoch: | 267.6904° |
| orbit number at epoch: | 92461 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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