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 25186.95825129 0.00000450 00000-0 60163-4 0 01
2 36125 98.0273 277.9328 0022474 215.4342 144.5656 14.79403887 08
| Epoch (UTC): | 05 July 2025 22:59:52 |
| Eccentricity: | 0.0022474 |
| inclination: | 98.0273° |
| perigee height: | 615 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 277.9328° |
| argument of perigee: | 215.4342° |
| revolutions per day: | 14.79403887 |
| mean anomaly at epoch: | 144.5656° |
| 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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