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 55392U 26145.47875825 +.00000000 +00000-0 +30947-4 0 00008
2 55392 69.9993 210.7314 0003674 268.7584 91.3155 14.98332942 08
| Epoch (UTC): | 25 May 2026 11:29:24 |
| Eccentricity: | 0.0003674 |
| inclination: | 69.9993° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 210.7314° |
| argument of perigee: | 268.7584° |
| revolutions per day: | 14.98332942 |
| mean anomaly at epoch: | 91.3155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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