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 26931U 01043C 25165.25630321 .00000156 00000-0 89400-4 0 9997
2 26931 67.0500 115.7490 0006064 276.1192 83.9218 14.31736973237773
| Epoch (UTC): | 14 June 2025 06:09:04 |
| Eccentricity: | 0.0006064 |
| inclination: | 67.0500° |
| perigee height: | 781 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 115.7490° |
| argument of perigee: | 276.1192° |
| revolutions per day: | 14.31736973 |
| mean anomaly at epoch: | 83.9218° |
| orbit number at epoch: | 23777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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