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 56025U 26145.60103200 +.00000000 +00000-0 +17091-4 0 00003
2 56025 43.0027 331.2433 0001035 253.0231 107.0508 15.27574413 00
| Epoch (UTC): | 25 May 2026 14:25:29 |
| Eccentricity: | 0.0001035 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.2433° |
| argument of perigee: | 253.0231° |
| revolutions per day: | 15.27574413 |
| mean anomaly at epoch: | 107.0508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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