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 36125U 09073B 25189.93422262 0.00000450 00000-0 60159-4 0 08
2 36125 98.0273 280.9041 0022474 205.8250 154.1749 14.79406564 00
| Epoch (UTC): | 08 July 2025 22:25:16 |
| Eccentricity: | 0.0022474 |
| inclination: | 98.0273° |
| perigee height: | 615 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 280.9041° |
| argument of perigee: | 205.8250° |
| revolutions per day: | 14.79406564 |
| mean anomaly at epoch: | 154.1749° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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