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 54143U 26145.41637419 +.00000000 +00000-0 -44958-2 0 00006
2 54143 87.9159 309.5027 0001628 88.2366 271.8954 13.19734355 01
| Epoch (UTC): | 25 May 2026 09:59:34 |
| Eccentricity: | 0.0001628 |
| inclination: | 87.9159° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5027° |
| argument of perigee: | 88.2366° |
| revolutions per day: | 13.19734355 |
| mean anomaly at epoch: | 271.8954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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