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 53224U 26145.42609446 +.00000000 +00000-0 -66849-3 0 00009
2 53224 97.4453 205.3197 0000432 111.9409 248.1865 15.05698788 02
| Epoch (UTC): | 25 May 2026 10:13:34 |
| Eccentricity: | 0.0000432 |
| inclination: | 97.4453° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 205.3197° |
| argument of perigee: | 111.9409° |
| revolutions per day: | 15.05698788 |
| mean anomaly at epoch: | 248.1865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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