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 55144U 26145.54592850 +.00000000 +00000-0 +58811-4 0 00005
2 55144 87.9159 339.9771 0001609 87.4398 272.6918 13.18685658 00
| Epoch (UTC): | 25 May 2026 13:06:08 |
| Eccentricity: | 0.0001609 |
| inclination: | 87.9159° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9771° |
| argument of perigee: | 87.4398° |
| revolutions per day: | 13.18685658 |
| mean anomaly at epoch: | 272.6918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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