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 63999U 26145.36451507 +.00000000 +00000-0 +11037-2 0 00002
2 63999 42.9998 284.7777 0000391 281.9669 78.1139 15.27594843 02
| Epoch (UTC): | 25 May 2026 08:44:54 |
| Eccentricity: | 0.0000391 |
| inclination: | 42.9998° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 284.7777° |
| argument of perigee: | 281.9669° |
| revolutions per day: | 15.27594843 |
| mean anomaly at epoch: | 78.1139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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