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 63551U 26145.62743044 +.00000000 +00000-0 +12813-2 0 00008
2 63551 42.9999 49.6235 0001281 269.5478 90.5243 15.70866527 06
| Epoch (UTC): | 25 May 2026 15:03:29 |
| Eccentricity: | 0.0001281 |
| inclination: | 42.9999° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 49.6235° |
| argument of perigee: | 269.5478° |
| revolutions per day: | 15.70866527 |
| mean anomaly at epoch: | 90.5243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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