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 51635U 26145.42777010 +.00000000 +00000-0 -20352-2 0 00004
2 51635 87.8849 40.7995 0001901 77.4648 282.6692 13.10373345 02
| Epoch (UTC): | 25 May 2026 10:15:59 |
| Eccentricity: | 0.0001901 |
| inclination: | 87.8849° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7995° |
| argument of perigee: | 77.4648° |
| revolutions per day: | 13.10373345 |
| mean anomaly at epoch: | 282.6692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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