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 66796U 26145.03640350 +.00000000 +00000-0 +53896-3 0 00000
2 66796 43.0007 28.3062 0001086 266.7092 93.3636 15.27569189 01
| Epoch (UTC): | 25 May 2026 00:52:25 |
| Eccentricity: | 0.0001086 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 28.3062° |
| argument of perigee: | 266.7092° |
| revolutions per day: | 15.27569189 |
| mean anomaly at epoch: | 93.3636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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