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 55104U 26145.62630439 +.00000000 +00000-0 +33265-3 0 00001
2 55104 97.3184 214.0940 0006342 168.5884 191.5512 15.48114065 03
| Epoch (UTC): | 25 May 2026 15:01:52 |
| Eccentricity: | 0.0006342 |
| inclination: | 97.3184° |
| perigee height: | 418 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 214.0940° |
| argument of perigee: | 168.5884° |
| revolutions per day: | 15.48114065 |
| mean anomaly at epoch: | 191.5512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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