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 53227U 26145.44125367 +.00000000 +00000-0 +68075-3 0 00001
2 53227 97.4544 206.4775 0001968 106.9198 253.2245 15.05723525 01
| Epoch (UTC): | 25 May 2026 10:35:24 |
| Eccentricity: | 0.0001968 |
| inclination: | 97.4544° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.4775° |
| argument of perigee: | 106.9198° |
| revolutions per day: | 15.05723525 |
| mean anomaly at epoch: | 253.2245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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