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 55861U 26145.54298198 +.00000000 +00000-0 +27352-3 0 00004
2 55861 97.3961 1.1124 0007038 78.0811 282.1232 15.55690140 00
| Epoch (UTC): | 25 May 2026 13:01:53 |
| Eccentricity: | 0.0007038 |
| inclination: | 97.3961° |
| perigee height: | 395 km |
| apogee height: | 405 km |
| right ascension of ascending node: | 1.1124° |
| argument of perigee: | 78.0811° |
| revolutions per day: | 15.55690140 |
| mean anomaly at epoch: | 282.1232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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