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 56552U 26145.47625948 +.00000000 +00000-0 +20140-3 0 00009
2 56552 43.0024 150.0993 0002010 279.1389 80.9236 15.27569110 02
| Epoch (UTC): | 25 May 2026 11:25:48 |
| Eccentricity: | 0.0002010 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.0993° |
| argument of perigee: | 279.1389° |
| revolutions per day: | 15.27569110 |
| mean anomaly at epoch: | 80.9236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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