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 63887U 26145.10770088 +.00000000 +00000-0 +89464-3 0 00008
2 63887 70.0016 41.6249 0002116 287.4094 72.6834 14.98352214 07
| Epoch (UTC): | 25 May 2026 02:35:05 |
| Eccentricity: | 0.0002116 |
| inclination: | 70.0016° |
| perigee height: | 571 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 41.6249° |
| argument of perigee: | 287.4094° |
| revolutions per day: | 14.98352214 |
| mean anomaly at epoch: | 72.6834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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