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 25199.08728158 .00000610 00000-0 74110-4 0 9993
2 29092 97.7724 222.4661 0001441 92.9793 267.1588 14.86978346 40245
| Epoch (UTC): | 18 July 2025 02:05:41 |
| Eccentricity: | 0.0001441 |
| inclination: | 97.7724° |
| perigee height: | 606 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 222.4661° |
| argument of perigee: | 92.9793° |
| revolutions per day: | 14.86978346 |
| mean anomaly at epoch: | 267.1588° |
| orbit number at epoch: | 4024 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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