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 51106U 26145.46392544 +.00000000 +00000-0 -10990-3 0 00004
2 51106 53.2140 304.4657 0001431 90.3105 269.8051 15.08845797 01
| Epoch (UTC): | 25 May 2026 11:08:03 |
| Eccentricity: | 0.0001431 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.4657° |
| argument of perigee: | 90.3105° |
| revolutions per day: | 15.08845797 |
| mean anomaly at epoch: | 269.8051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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