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 54142U 26145.36792447 +.00000000 +00000-0 -29562-3 0 00007
2 54142 87.9176 278.9868 0001691 127.6752 232.4535 13.20770445 08
| Epoch (UTC): | 25 May 2026 08:49:48 |
| Eccentricity: | 0.0001691 |
| inclination: | 87.9176° |
| perigee height: | 1181 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9868° |
| argument of perigee: | 127.6752° |
| revolutions per day: | 13.20770445 |
| mean anomaly at epoch: | 232.4535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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