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 56818U 26145.39045324 +.00000000 +00000-0 +30714-3 0 00007
2 56818 70.0000 150.8883 0003256 268.4274 91.6512 14.98333901 04
| Epoch (UTC): | 25 May 2026 09:22:15 |
| Eccentricity: | 0.0003256 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 150.8883° |
| argument of perigee: | 268.4274° |
| revolutions per day: | 14.98333901 |
| mean anomaly at epoch: | 91.6512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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