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 23151.06271170 .00000823 00000-0 10482-3 0 9991
2 29092 97.8390 178.5823 0001516 92.4317 267.7071 14.84134441924585
| Epoch (UTC): | 31 May 2023 01:30:18 |
| Eccentricity: | 0.0001516 |
| inclination: | 97.8390° |
| perigee height: | 615 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 178.5823° |
| argument of perigee: | 92.4317° |
| revolutions per day: | 14.84134441 |
| mean anomaly at epoch: | 267.7071° |
| orbit number at epoch: | 92458 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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