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 51627U 26145.36387556 +.00000000 +00000-0 -20508-3 0 00004
2 51627 87.9155 10.4022 0001945 84.2379 275.8974 13.17648322 08
| Epoch (UTC): | 25 May 2026 08:43:58 |
| Eccentricity: | 0.0001945 |
| inclination: | 87.9155° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4022° |
| argument of perigee: | 84.2379° |
| revolutions per day: | 13.17648322 |
| mean anomaly at epoch: | 275.8974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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