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 56007U 26145.61066115 +.00000000 +00000-0 +25837-4 0 00004
2 56007 43.0048 345.1829 0001707 273.9034 86.1623 15.27574087 06
| Epoch (UTC): | 25 May 2026 14:39:21 |
| Eccentricity: | 0.0001707 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.1829° |
| argument of perigee: | 273.9034° |
| revolutions per day: | 15.27574087 |
| mean anomaly at epoch: | 86.1623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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