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 53655U 26145.66668980 +.00000000 +00000-0 +19174-1 0 00007
2 53655 97.6015 28.8649 0001940 65.0314 43.2143 15.42997748 07
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001940 |
| inclination: | 97.6015° |
| perigee height: | 436 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 28.8649° |
| argument of perigee: | 65.0314° |
| revolutions per day: | 15.42997748 |
| mean anomaly at epoch: | 43.2143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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