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 56955U 26145.37521507 +.00000000 +00000-0 +32040-3 0 00003
2 56955 97.6175 280.4847 0002154 87.3457 272.8024 15.18275082 00
| Epoch (UTC): | 25 May 2026 09:00:18 |
| Eccentricity: | 0.0002154 |
| inclination: | 97.6175° |
| perigee height: | 510 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 280.4847° |
| argument of perigee: | 87.3457° |
| revolutions per day: | 15.18275082 |
| mean anomaly at epoch: | 272.8024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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