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 51624U 26145.40786459 +.00000000 +00000-0 +29148-3 0 00009
2 51624 87.8849 40.8000 0001591 84.4511 275.6798 13.10370287 01
| Epoch (UTC): | 25 May 2026 09:47:19 |
| Eccentricity: | 0.0001591 |
| inclination: | 87.8849° |
| perigee height: | 1221 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8000° |
| argument of perigee: | 84.4511° |
| revolutions per day: | 13.10370287 |
| mean anomaly at epoch: | 275.6798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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