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 56062U 26145.51583069 +.00000000 +00000-0 -52996-5 0 00004
2 56062 87.9103 233.2725 0002265 105.6920 254.4461 13.16592980 01
| Epoch (UTC): | 25 May 2026 12:22:47 |
| Eccentricity: | 0.0002265 |
| inclination: | 87.9103° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2725° |
| argument of perigee: | 105.6920° |
| revolutions per day: | 13.16592980 |
| mean anomaly at epoch: | 254.4461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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