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 54381U 26145.52325756 +.00000000 +00000-0 +36048-4 0 00002
2 54381 67.1467 162.3395 0006569 275.1782 84.8553 13.96676451 02
| Epoch (UTC): | 25 May 2026 12:33:29 |
| Eccentricity: | 0.0006569 |
| inclination: | 67.1467° |
| perigee height: | 901 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 162.3395° |
| argument of perigee: | 275.1782° |
| revolutions per day: | 13.96676451 |
| mean anomaly at epoch: | 84.8553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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