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 56944U 26145.62485226 +.00000000 +00000-0 +37402-3 0 00003
2 56944 97.5484 281.9798 0007778 50.9533 309.2398 15.30005658 02
| Epoch (UTC): | 25 May 2026 14:59:47 |
| Eccentricity: | 0.0007778 |
| inclination: | 97.5484° |
| perigee height: | 470 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 281.9798° |
| argument of perigee: | 50.9533° |
| revolutions per day: | 15.30005658 |
| mean anomaly at epoch: | 309.2398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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