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 55313U 26145.47830558 +.00000000 +00000-0 +30499-4 0 00007
2 55313 69.9988 170.8767 0003696 267.2392 92.8345 14.98330304 05
| Epoch (UTC): | 25 May 2026 11:28:45 |
| Eccentricity: | 0.0003696 |
| inclination: | 69.9988° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 170.8767° |
| argument of perigee: | 267.2392° |
| revolutions per day: | 14.98330304 |
| mean anomaly at epoch: | 92.8345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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