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 63719U 26145.48781956 +.00000000 +00000-0 +65400-3 0 00003
2 63719 53.1593 221.7121 0001283 79.6423 280.4725 15.34403884 03
| Epoch (UTC): | 25 May 2026 11:42:27 |
| Eccentricity: | 0.0001283 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 221.7121° |
| argument of perigee: | 79.6423° |
| revolutions per day: | 15.34403884 |
| mean anomaly at epoch: | 280.4725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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