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 41787U 26145.43344670 +.00000000 +00000-0 +10045-3 0 00002
2 41787 97.8167 145.7373 0026940 279.4398 80.3763 14.67631896 08
| Epoch (UTC): | 25 May 2026 10:24:09 |
| Eccentricity: | 0.0026940 |
| inclination: | 97.8167° |
| perigee height: | 650 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 145.7373° |
| argument of perigee: | 279.4398° |
| revolutions per day: | 14.67631896 |
| mean anomaly at epoch: | 80.3763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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