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 56056U 26145.52217023 +.00000000 +00000-0 +96907-4 0 00000
2 56056 87.9103 233.2834 0002272 96.0945 264.0445 13.16593429 01
| Epoch (UTC): | 25 May 2026 12:31:55 |
| Eccentricity: | 0.0002272 |
| inclination: | 87.9103° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2834° |
| argument of perigee: | 96.0945° |
| revolutions per day: | 13.16593429 |
| mean anomaly at epoch: | 264.0445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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