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 52763U 26145.39739468 +.00000000 +00000-0 +21557-3 0 00006
2 52763 97.6657 293.6844 0008129 164.1791 195.9707 15.35891808 06
| Epoch (UTC): | 25 May 2026 09:32:14 |
| Eccentricity: | 0.0008129 |
| inclination: | 97.6657° |
| perigee height: | 453 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 293.6844° |
| argument of perigee: | 164.1791° |
| revolutions per day: | 15.35891808 |
| mean anomaly at epoch: | 195.9707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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