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 29528U 06051C 25196.54701134 -.00000074 00000-0 -19909-3 0 9990
2 29528 51.4285 24.2501 6002062 28.0265 359.7474 3.64297851248622
| Epoch (UTC): | 15 July 2025 13:07:41 |
| Eccentricity: | 0.6002062 |
| inclination: | 51.4285° |
| perigee height: | 755 km |
| apogee height: | 22171 km |
| right ascension of ascending node: | 24.2501° |
| argument of perigee: | 28.0265° |
| revolutions per day: | 3.64297851 |
| mean anomaly at epoch: | 359.7474° |
| orbit number at epoch: | 24862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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