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 55093U 26145.59738023 +.00000000 +00000-0 +22371-3 0 00008
2 55093 97.3261 212.7748 0010504 155.8727 204.3013 15.39616159 07
| Epoch (UTC): | 25 May 2026 14:20:13 |
| Eccentricity: | 0.0010504 |
| inclination: | 97.3261° |
| perigee height: | 440 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 212.7748° |
| argument of perigee: | 155.8727° |
| revolutions per day: | 15.39616159 |
| mean anomaly at epoch: | 204.3013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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