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 51719U 26145.57801943 +.00000000 +00000-0 +23394-4 0 00006
2 51719 53.2118 344.0330 0001123 84.2644 275.8476 15.08833643 07
| Epoch (UTC): | 25 May 2026 13:52:20 |
| Eccentricity: | 0.0001123 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 344.0330° |
| argument of perigee: | 84.2644° |
| revolutions per day: | 15.08833643 |
| mean anomaly at epoch: | 275.8476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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