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 53685U 26145.41918613 +.00000000 +00000-0 +11475-3 0 00002
2 53685 97.4518 25.2987 0002553 79.4019 280.7496 15.05652396 09
| Epoch (UTC): | 25 May 2026 10:03:37 |
| Eccentricity: | 0.0002553 |
| inclination: | 97.4518° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.2987° |
| argument of perigee: | 79.4019° |
| revolutions per day: | 15.05652396 |
| mean anomaly at epoch: | 280.7496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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