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 53204U 26145.66668980 +.00000000 +00000-0 +26904-2 0 00007
2 53204 97.6009 206.3584 0001844 61.4623 306.6600 15.22482334 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001844 |
| inclination: | 97.6009° |
| perigee height: | 497 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 206.3584° |
| argument of perigee: | 61.4623° |
| revolutions per day: | 15.22482334 |
| mean anomaly at epoch: | 306.6600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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