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 63871U 26145.11587176 +.00000000 +00000-0 +24392-3 0 00005
2 63871 70.0015 41.6653 0002831 269.0599 91.0236 14.98337104 00
| Epoch (UTC): | 25 May 2026 02:46:51 |
| Eccentricity: | 0.0002831 |
| inclination: | 70.0015° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.6653° |
| argument of perigee: | 269.0599° |
| revolutions per day: | 14.98337104 |
| mean anomaly at epoch: | 91.0236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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