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 54671U 26145.56863786 +.00000000 +00000-0 -89765-4 0 00003
2 54671 87.9260 248.4691 0002038 95.9451 264.1915 13.21827735 04
| Epoch (UTC): | 25 May 2026 13:38:50 |
| Eccentricity: | 0.0002038 |
| inclination: | 87.9260° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4691° |
| argument of perigee: | 95.9451° |
| revolutions per day: | 13.21827735 |
| mean anomaly at epoch: | 264.1915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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