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 53231U 26145.43577086 +.00000000 +00000-0 -10346-3 0 00003
2 53231 97.4512 206.4893 0000937 119.2116 240.9205 15.05653243 02
| Epoch (UTC): | 25 May 2026 10:27:30 |
| Eccentricity: | 0.0000937 |
| inclination: | 97.4512° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 206.4893° |
| argument of perigee: | 119.2116° |
| revolutions per day: | 15.05653243 |
| mean anomaly at epoch: | 240.9205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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