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 63287U 26145.36491939 +.00000000 +00000-0 +62057-3 0 00004
2 63287 43.0010 168.4324 0001226 270.6081 89.4630 15.27586094 06
| Epoch (UTC): | 25 May 2026 08:45:29 |
| Eccentricity: | 0.0001226 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.4324° |
| argument of perigee: | 270.6081° |
| revolutions per day: | 15.27586094 |
| mean anomaly at epoch: | 89.4630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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