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 56030U 26145.50351889 +.00000000 +00000-0 +55937-5 0 00008
2 56030 43.0057 331.3744 0001884 272.4173 87.6463 15.27575366 08
| Epoch (UTC): | 25 May 2026 12:05:04 |
| Eccentricity: | 0.0001884 |
| inclination: | 43.0057° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.3744° |
| argument of perigee: | 272.4173° |
| revolutions per day: | 15.27575366 |
| mean anomaly at epoch: | 87.6463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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