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 10521U 77119B 25189.78365656 .00000106 00000-0 40194-4 0 9994
2 10521 74.0248 216.1040 0021399 233.9432 125.9742 14.42191915495959
| Epoch (UTC): | 08 July 2025 18:48:27 |
| Eccentricity: | 0.0021399 |
| inclination: | 74.0248° |
| perigee height: | 736 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 216.1040° |
| argument of perigee: | 233.9432° |
| revolutions per day: | 14.42191915 |
| mean anomaly at epoch: | 125.9742° |
| orbit number at epoch: | 49595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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