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 56345U 26145.46626102 +.00000000 +00000-0 +73471-4 0 00007
2 56345 97.4473 145.3674 0002204 93.7998 266.3481 15.05648490 04
| Epoch (UTC): | 25 May 2026 11:11:24 |
| Eccentricity: | 0.0002204 |
| inclination: | 97.4473° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.3674° |
| argument of perigee: | 93.7998° |
| revolutions per day: | 15.05648490 |
| mean anomaly at epoch: | 266.3481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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