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 65533U 26145.62188860 +.00000000 +00000-0 +30707-3 0 00002
2 65533 97.4491 215.2030 0004943 133.0677 227.0965 15.05675910 08
| Epoch (UTC): | 25 May 2026 14:55:31 |
| Eccentricity: | 0.0004943 |
| inclination: | 97.4491° |
| perigee height: | 546 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 215.2030° |
| argument of perigee: | 133.0677° |
| revolutions per day: | 15.05675910 |
| mean anomaly at epoch: | 227.0965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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