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 53688U 26145.39426860 +.00000000 +00000-0 +33512-3 0 00006
2 53688 97.4500 25.3136 0002027 92.5455 267.6005 15.05627695 00
| Epoch (UTC): | 25 May 2026 09:27:44 |
| Eccentricity: | 0.0002027 |
| inclination: | 97.4500° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.3136° |
| argument of perigee: | 92.5455° |
| revolutions per day: | 15.05627695 |
| mean anomaly at epoch: | 267.6005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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