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 53495U 26145.29735716 +.00000000 +00000-0 +10366-4 0 00007
2 53495 97.4472 265.2183 0001060 112.8964 247.2375 15.05658749 06
| Epoch (UTC): | 25 May 2026 07:08:11 |
| Eccentricity: | 0.0001060 |
| inclination: | 97.4472° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 265.2183° |
| argument of perigee: | 112.8964° |
| revolutions per day: | 15.05658749 |
| mean anomaly at epoch: | 247.2375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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