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 53654U 26145.63100117 +.00000000 +00000-0 +73960-3 0 00001
2 53654 97.4497 26.6294 0001927 80.7808 279.3637 15.05605329 07
| Epoch (UTC): | 25 May 2026 15:08:38 |
| Eccentricity: | 0.0001927 |
| inclination: | 97.4497° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.6294° |
| argument of perigee: | 80.7808° |
| revolutions per day: | 15.05605329 |
| mean anomaly at epoch: | 279.3637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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