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 56996U 26145.52860198 +.00000000 +00000-0 +41988-3 0 00008
2 56996 98.1451 284.9065 0057471 170.4121 189.8204 14.85335684 08
| Epoch (UTC): | 25 May 2026 12:41:11 |
| Eccentricity: | 0.0057471 |
| inclination: | 98.1451° |
| perigee height: | 572 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 284.9065° |
| argument of perigee: | 170.4121° |
| revolutions per day: | 14.85335684 |
| mean anomaly at epoch: | 189.8204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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