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 63735U 26145.63635164 +.00000000 +00000-0 +45099-4 0 00000
2 63735 51.9016 122.8405 0001225 4.2730 355.8243 14.79942512 00
| Epoch (UTC): | 25 May 2026 15:16:20 |
| Eccentricity: | 0.0001225 |
| inclination: | 51.9016° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 122.8405° |
| argument of perigee: | 4.2730° |
| revolutions per day: | 14.79942512 |
| mean anomaly at epoch: | 355.8243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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