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 25682U 26150.49009647 +.00000000 +00000-0 +11291-3 0 00006
2 25682 97.8579 154.9372 0001702 99.4526 55.7253 14.63899934 09
| Epoch (UTC): | 30 May 2026 11:45:44 |
| Eccentricity: | 0.0001702 |
| inclination: | 97.8579° |
| perigee height: | 679 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 154.9372° |
| argument of perigee: | 99.4526° |
| revolutions per day: | 14.63899934 |
| mean anomaly at epoch: | 55.7253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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