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 23150.52334672 .00000835 00000-0 10625-3 0 9990
2 29092 97.8391 178.0522 0001530 92.5882 267.5507 14.84133501924400
| Epoch (UTC): | 30 May 2023 12:33:37 |
| Eccentricity: | 0.0001530 |
| inclination: | 97.8391° |
| perigee height: | 615 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 178.0522° |
| argument of perigee: | 92.5882° |
| revolutions per day: | 14.84133501 |
| mean anomaly at epoch: | 267.5507° |
| orbit number at epoch: | 92440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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