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 55430U 26145.41684628 +.00000000 +00000-0 +18030-3 0 00002
2 55430 69.9995 270.9157 0003076 267.7746 92.3061 14.98346062 06
| Epoch (UTC): | 25 May 2026 10:00:15 |
| Eccentricity: | 0.0003076 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 270.9157° |
| argument of perigee: | 267.7746° |
| revolutions per day: | 14.98346062 |
| mean anomaly at epoch: | 92.3061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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