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 51887U 26145.59732779 +.00000000 +00000-0 -23680-4 0 00003
2 51887 53.2102 13.8678 0001982 90.9271 269.1948 15.08844563 08
| Epoch (UTC): | 25 May 2026 14:20:09 |
| Eccentricity: | 0.0001982 |
| inclination: | 53.2102° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 13.8678° |
| argument of perigee: | 90.9271° |
| revolutions per day: | 15.08844563 |
| mean anomaly at epoch: | 269.1948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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