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 63147U 26144.80232257 +.00000000 +00000-0 +42527-3 0 00003
2 63147 42.9992 313.2414 0001766 259.5304 100.5349 15.27588409 05
| Epoch (UTC): | 24 May 2026 19:15:20 |
| Eccentricity: | 0.0001766 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.2414° |
| argument of perigee: | 259.5304° |
| revolutions per day: | 15.27588409 |
| mean anomaly at epoch: | 100.5349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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