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 55641U 26145.30100139 +.00000000 +00000-0 +63417-4 0 00004
2 55641 69.9996 351.4266 0003120 266.9184 93.1618 14.98325330 06
| Epoch (UTC): | 25 May 2026 07:13:26 |
| Eccentricity: | 0.0003120 |
| inclination: | 69.9996° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 351.4266° |
| argument of perigee: | 266.9184° |
| revolutions per day: | 14.98325330 |
| mean anomaly at epoch: | 93.1618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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