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 28116U 03056E 25198.23295473 .00001571 00000-0 52103-3 0 9990
2 28116 52.9553 285.2838 5675538 264.1239 32.2354 4.50095760343264
| Epoch (UTC): | 17 July 2025 05:35:27 |
| Eccentricity: | 0.5675538 |
| inclination: | 52.9553° |
| perigee height: | 323 km |
| apogee height: | 17911 km |
| right ascension of ascending node: | 285.2838° |
| argument of perigee: | 264.1239° |
| revolutions per day: | 4.50095760 |
| mean anomaly at epoch: | 32.2354° |
| orbit number at epoch: | 34326 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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