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 53687U 26145.46207213 +.00000000 +00000-0 -13074-3 0 00004
2 53687 97.4471 26.4560 0002208 100.0154 260.1322 15.05658685 04
| Epoch (UTC): | 25 May 2026 11:05:23 |
| Eccentricity: | 0.0002208 |
| inclination: | 97.4471° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.4560° |
| argument of perigee: | 100.0154° |
| revolutions per day: | 15.05658685 |
| mean anomaly at epoch: | 260.1322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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