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 56341U 26145.51610941 +.00000000 +00000-0 +10645-3 0 00006
2 56341 97.4459 145.4520 0002365 87.2549 272.8949 15.05640739 02
| Epoch (UTC): | 25 May 2026 12:23:11 |
| Eccentricity: | 0.0002365 |
| inclination: | 97.4459° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.4520° |
| argument of perigee: | 87.2549° |
| revolutions per day: | 15.05640739 |
| mean anomaly at epoch: | 272.8949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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