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 25131.38373096 .00000165 00000-0 61255-4 0 9991
2 13028 74.0388 111.3144 0019870 203.9602 156.0630 14.39656929271766
| Epoch (UTC): | 11 May 2025 09:12:34 |
| Eccentricity: | 0.0019870 |
| inclination: | 74.0388° |
| perigee height: | 745 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 111.3144° |
| argument of perigee: | 203.9602° |
| revolutions per day: | 14.39656929 |
| mean anomaly at epoch: | 156.0630° |
| orbit number at epoch: | 27176 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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