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 55143U 26145.47680934 +.00000000 +00000-0 +50115-2 0 00004
2 55143 87.9159 339.9911 0001663 81.3948 278.7372 13.18677984 03
| Epoch (UTC): | 25 May 2026 11:26:36 |
| Eccentricity: | 0.0001663 |
| inclination: | 87.9159° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9911° |
| argument of perigee: | 81.3948° |
| revolutions per day: | 13.18677984 |
| mean anomaly at epoch: | 278.7372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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