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 56480U 26145.57850764 +.00000000 +00000-0 +51094-3 0 00008
2 56480 69.9917 249.9521 0003308 283.2059 76.8750 15.36141827 02
| Epoch (UTC): | 25 May 2026 13:53:03 |
| Eccentricity: | 0.0003308 |
| inclination: | 69.9917° |
| perigee height: | 455 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 249.9521° |
| argument of perigee: | 283.2059° |
| revolutions per day: | 15.36141827 |
| mean anomaly at epoch: | 76.8750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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