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 55056U 26145.61685549 +.00000000 +00000-0 +27863-3 0 00005
2 55056 97.3236 216.3959 0005085 200.3578 159.7477 15.59121520 02
| Epoch (UTC): | 25 May 2026 14:48:16 |
| Eccentricity: | 0.0005085 |
| inclination: | 97.3236° |
| perigee height: | 387 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 216.3959° |
| argument of perigee: | 200.3578° |
| revolutions per day: | 15.59121520 |
| mean anomaly at epoch: | 159.7477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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