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 63951U 26145.52523677 +.00000000 +00000-0 +12619-3 0 00004
2 63951 70.0010 80.6460 0003552 257.9630 102.1131 14.98335222 03
| Epoch (UTC): | 25 May 2026 12:36:20 |
| Eccentricity: | 0.0003552 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 80.6460° |
| argument of perigee: | 257.9630° |
| revolutions per day: | 14.98335222 |
| mean anomaly at epoch: | 102.1131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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