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 56956U 26145.62684544 +.00000000 +00000-0 +30212-3 0 00002
2 56956 97.6164 280.5144 0001470 95.0384 265.1018 15.18262476 06
| Epoch (UTC): | 25 May 2026 15:02:39 |
| Eccentricity: | 0.0001470 |
| inclination: | 97.6164° |
| perigee height: | 510 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 280.5144° |
| argument of perigee: | 95.0384° |
| revolutions per day: | 15.18262476 |
| mean anomaly at epoch: | 265.1018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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