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 56482U 26145.42127652 +.00000000 +00000-0 +38648-4 0 00008
2 56482 69.9985 290.9564 0003181 268.3794 91.7001 14.98321599 09
| Epoch (UTC): | 25 May 2026 10:06:38 |
| Eccentricity: | 0.0003181 |
| inclination: | 69.9985° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 290.9564° |
| argument of perigee: | 268.3794° |
| revolutions per day: | 14.98321599 |
| mean anomaly at epoch: | 91.7001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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