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 54642U 26145.53750522 +.00000000 +00000-0 -43870-3 0 00007
2 54642 87.9251 248.5014 0001947 101.8771 258.2582 13.21826098 07
| Epoch (UTC): | 25 May 2026 12:54:00 |
| Eccentricity: | 0.0001947 |
| inclination: | 87.9251° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.5014° |
| argument of perigee: | 101.8771° |
| revolutions per day: | 13.21826098 |
| mean anomaly at epoch: | 258.2582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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