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 54665U 26145.55181260 +.00000000 +00000-0 +83440-4 0 00008
2 54665 87.9251 248.4990 0002259 98.1171 262.0219 13.21828082 08
| Epoch (UTC): | 25 May 2026 13:14:36 |
| Eccentricity: | 0.0002259 |
| inclination: | 87.9251° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4990° |
| argument of perigee: | 98.1171° |
| revolutions per day: | 13.21828082 |
| mean anomaly at epoch: | 262.0219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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