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 53663U 26145.38733227 +.00000000 +00000-0 +13499-2 0 00007
2 53663 97.4475 26.4795 0002205 81.4999 278.6478 15.05550613 06
| Epoch (UTC): | 25 May 2026 09:17:45 |
| Eccentricity: | 0.0002205 |
| inclination: | 97.4475° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.4795° |
| argument of perigee: | 81.4999° |
| revolutions per day: | 15.05550613 |
| mean anomaly at epoch: | 278.6478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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