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 51742U 26145.54951208 +.00000000 +00000-0 -44161-5 0 00006
2 51742 53.2108 334.2760 0001388 88.3928 271.7223 15.08837939 00
| Epoch (UTC): | 25 May 2026 13:11:17 |
| Eccentricity: | 0.0001388 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.2760° |
| argument of perigee: | 88.3928° |
| revolutions per day: | 15.08837939 |
| mean anomaly at epoch: | 271.7223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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