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 55944U 26145.26458087 +.00000000 +00000-0 +96834-4 0 00002
2 55944 69.9997 91.2530 0003377 265.6538 94.4236 14.98335115 01
| Epoch (UTC): | 25 May 2026 06:20:59 |
| Eccentricity: | 0.0003377 |
| inclination: | 69.9997° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.2530° |
| argument of perigee: | 265.6538° |
| revolutions per day: | 14.98335115 |
| mean anomaly at epoch: | 94.4236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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