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 55662U 26144.93418823 +.00000000 +00000-0 -12809-4 0 00007
2 55662 69.9994 332.2920 0002449 267.1946 92.8933 14.97525564 09
| Epoch (UTC): | 24 May 2026 22:25:13 |
| Eccentricity: | 0.0002449 |
| inclination: | 69.9994° |
| perigee height: | 573 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 332.2920° |
| argument of perigee: | 267.1946° |
| revolutions per day: | 14.97525564 |
| mean anomaly at epoch: | 92.8933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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