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 65567U 26145.64379222 +.00000000 +00000-0 +91389-4 0 00009
2 65567 81.3070 31.9294 0004557 263.4747 96.5890 13.83043594 09
| Epoch (UTC): | 25 May 2026 15:27:03 |
| Eccentricity: | 0.0004557 |
| inclination: | 81.3070° |
| perigee height: | 950 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 31.9294° |
| argument of perigee: | 263.4747° |
| revolutions per day: | 13.83043594 |
| mean anomaly at epoch: | 96.5890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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