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 51888U 26145.60470139 +.00000000 +00000-0 +10137-3 0 00006
2 51888 53.2142 13.8355 0001481 95.8874 264.2287 15.08841070 04
| Epoch (UTC): | 25 May 2026 14:30:46 |
| Eccentricity: | 0.0001481 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 13.8355° |
| argument of perigee: | 95.8874° |
| revolutions per day: | 15.08841070 |
| mean anomaly at epoch: | 264.2287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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