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 55916U 26145.32740766 +.00000000 +00000-0 -10391-3 0 00000
2 55916 69.9995 111.3537 0004033 263.5517 96.5183 14.98327914 05
| Epoch (UTC): | 25 May 2026 07:51:28 |
| Eccentricity: | 0.0004033 |
| inclination: | 69.9995° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 111.3537° |
| argument of perigee: | 263.5517° |
| revolutions per day: | 14.98327914 |
| mean anomaly at epoch: | 96.5183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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