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 56454U 26145.17952008 +.00000000 +00000-0 +59801-4 0 00004
2 56454 69.9991 311.5900 0003086 266.8247 93.2559 14.98329408 01
| Epoch (UTC): | 25 May 2026 04:18:30 |
| Eccentricity: | 0.0003086 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 311.5900° |
| argument of perigee: | 266.8247° |
| revolutions per day: | 14.98329408 |
| mean anomaly at epoch: | 93.2559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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