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 51630U 26145.45586399 +.00000000 +00000-0 +12146-2 0 00001
2 51630 87.8858 40.7916 0001201 76.2710 283.8551 13.10376291 00
| Epoch (UTC): | 25 May 2026 10:56:26 |
| Eccentricity: | 0.0001201 |
| inclination: | 87.8858° |
| perigee height: | 1221 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7916° |
| argument of perigee: | 76.2710° |
| revolutions per day: | 13.10376291 |
| mean anomaly at epoch: | 283.8551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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