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 54664U 26145.56023000 +.00000000 +00000-0 +17206-3 0 00001
2 54664 87.9251 248.4810 0001935 93.6208 266.5147 13.21827616 00
| Epoch (UTC): | 25 May 2026 13:26:43 |
| Eccentricity: | 0.0001935 |
| inclination: | 87.9251° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4810° |
| argument of perigee: | 93.6208° |
| revolutions per day: | 13.21827616 |
| mean anomaly at epoch: | 266.5147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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