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 63450U 26145.43131309 +.00000000 +00000-0 +67226-3 0 00009
2 63450 53.1578 143.2178 0001064 77.0527 283.0598 15.42180570 02
| Epoch (UTC): | 25 May 2026 10:21:05 |
| Eccentricity: | 0.0001064 |
| inclination: | 53.1578° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.2178° |
| argument of perigee: | 77.0527° |
| revolutions per day: | 15.42180570 |
| mean anomaly at epoch: | 283.0598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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