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 25544U 26106.84451399 +.00000000 +00000-0 +85733-4 0 00001
2 25544 51.6329 243.6903 0006573 315.5681 44.4780 15.48789484 00
| Epoch (UTC): | 16 April 2026 20:16:06 |
| Eccentricity: | 0.0006573 |
| inclination: | 51.6329° |
| perigee height: | 416 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 243.6903° |
| argument of perigee: | 315.5681° |
| revolutions per day: | 15.48789484 |
| mean anomaly at epoch: | 44.4780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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