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 63893U 26145.36545157 +.00000000 +00000-0 -36290-3 0 00000
2 63893 42.9981 103.2564 0000805 259.7266 100.3495 15.27541049 05
| Epoch (UTC): | 25 May 2026 08:46:15 |
| Eccentricity: | 0.0000805 |
| inclination: | 42.9981° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.2564° |
| argument of perigee: | 259.7266° |
| revolutions per day: | 15.27541049 |
| mean anomaly at epoch: | 100.3495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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