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 55360U 26145.57802826 +.00000000 +00000-0 +76012-5 0 00009
2 55360 43.0009 247.1791 0001297 275.1475 84.9228 15.27572582 05
| Epoch (UTC): | 25 May 2026 13:52:21 |
| Eccentricity: | 0.0001297 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.1791° |
| argument of perigee: | 275.1475° |
| revolutions per day: | 15.27572582 |
| mean anomaly at epoch: | 84.9228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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