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 55380U 26145.51093728 +.00000000 +00000-0 +34789-2 0 00000
2 55380 42.9995 228.3278 0001266 276.4743 83.5957 15.06021105 09
| Epoch (UTC): | 25 May 2026 12:15:44 |
| Eccentricity: | 0.0001266 |
| inclination: | 42.9995° |
| perigee height: | 547 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 228.3278° |
| argument of perigee: | 276.4743° |
| revolutions per day: | 15.06021105 |
| mean anomaly at epoch: | 83.5957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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