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 51788U 26145.61664882 +.00000000 +00000-0 +28616-4 0 00008
2 51788 53.2122 3.7825 0001359 93.9701 266.1447 15.08836325 09
| Epoch (UTC): | 25 May 2026 14:47:58 |
| Eccentricity: | 0.0001359 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 3.7825° |
| argument of perigee: | 93.9701° |
| revolutions per day: | 15.08836325 |
| mean anomaly at epoch: | 266.1447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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