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 is defined by the following mean orbital elements,
1 39768U 26150.29596639 +.00000000 +00000-0 +21411-3 0 00001
2 39768 97.9058 263.6176 0006949 48.0895 312.0916 14.94712765 04
| Epoch (UTC): | 30 May 2026 07:06:11 |
| Eccentricity: | 0.0006949 |
| inclination: | 97.9058° |
| perigee height: | 578 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 263.6176° |
| argument of perigee: | 48.0895° |
| revolutions per day: | 14.94712765 |
| mean anomaly at epoch: | 312.0916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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