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 55783U 26145.60998370 +.00000000 +00000-0 -97157-5 0 00006
2 55783 70.0004 10.6935 0002725 268.8105 91.2741 14.98328678 01
| Epoch (UTC): | 25 May 2026 14:38:22 |
| Eccentricity: | 0.0002725 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 10.6935° |
| argument of perigee: | 268.8105° |
| revolutions per day: | 14.98328678 |
| mean anomaly at epoch: | 91.2741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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