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 63397U 26145.80054919 +.00000000 +00000-0 +00000-0 0 00005
2 63397 1.0426 81.5628 0004068 288.0420 322.5392 1.00272505 03
| Epoch (UTC): | 25 May 2026 19:12:47 |
| Eccentricity: | 0.0004068 |
| inclination: | 1.0426° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 81.5628° |
| argument of perigee: | 288.0420° |
| revolutions per day: | 1.00272505 |
| mean anomaly at epoch: | 322.5392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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