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 55938U 26145.55667456 +.00000000 +00000-0 -18037-3 0 00008
2 55938 70.0004 90.6709 0003265 268.4482 91.6303 14.98321605 05
| Epoch (UTC): | 25 May 2026 13:21:36 |
| Eccentricity: | 0.0003265 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 90.6709° |
| argument of perigee: | 268.4482° |
| revolutions per day: | 14.98321605 |
| mean anomaly at epoch: | 91.6303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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