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 55135U 26145.50232191 +.00000000 +00000-0 +34697-3 0 00005
2 55135 97.1531 222.0548 0003378 179.2738 180.8522 15.54510718 01
| Epoch (UTC): | 25 May 2026 12:03:20 |
| Eccentricity: | 0.0003378 |
| inclination: | 97.1531° |
| perigee height: | 401 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 222.0548° |
| argument of perigee: | 179.2738° |
| revolutions per day: | 15.54510718 |
| mean anomaly at epoch: | 180.8522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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