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 51625U 26145.41946625 +.00000000 +00000-0 -16889-2 0 00002
2 51625 87.8848 40.8167 0001656 93.3270 266.8047 13.10370745 06
| Epoch (UTC): | 25 May 2026 10:04:01 |
| Eccentricity: | 0.0001656 |
| inclination: | 87.8848° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8167° |
| argument of perigee: | 93.3270° |
| revolutions per day: | 13.10370745 |
| mean anomaly at epoch: | 266.8047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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