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 55634U 26145.56840954 +.00000000 +00000-0 +12274-3 0 00004
2 55634 69.9997 10.6292 0003590 265.1778 94.8971 14.98334893 07
| Epoch (UTC): | 25 May 2026 13:38:30 |
| Eccentricity: | 0.0003590 |
| inclination: | 69.9997° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 10.6292° |
| argument of perigee: | 265.1778° |
| revolutions per day: | 14.98334893 |
| mean anomaly at epoch: | 94.8971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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