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 13028U 82001B 25194.68759256 .00000192 00000-0 69703-4 0 9995
2 13028 74.0415 354.4402 0018463 66.8348 293.4749 14.39689184281143
| Epoch (UTC): | 13 July 2025 16:30:07 |
| Eccentricity: | 0.0018463 |
| inclination: | 74.0415° |
| perigee height: | 746 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 354.4402° |
| argument of perigee: | 66.8348° |
| revolutions per day: | 14.39689184 |
| mean anomaly at epoch: | 293.4749° |
| orbit number at epoch: | 28114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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