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 25191.96329626 0.00000350 00000-0 46790-4 0 08
2 36125 98.0273 282.9300 0022474 199.2733 160.7266 14.79406981 02
| Epoch (UTC): | 10 July 2025 23:07:08 |
| Eccentricity: | 0.0022474 |
| inclination: | 98.0273° |
| perigee height: | 615 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 282.9300° |
| argument of perigee: | 199.2733° |
| revolutions per day: | 14.79406981 |
| mean anomaly at epoch: | 160.7266° |
| 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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