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 63444U 26145.43287262 +.00000000 +00000-0 +76911-3 0 00003
2 63444 53.1580 143.2273 0000775 105.1146 254.9946 15.42186370 00
| Epoch (UTC): | 25 May 2026 10:23:20 |
| Eccentricity: | 0.0000775 |
| inclination: | 53.1580° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.2273° |
| argument of perigee: | 105.1146° |
| revolutions per day: | 15.42186370 |
| mean anomaly at epoch: | 254.9946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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