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 63010U 26145.25427751 +.00000000 +00000-0 +21766-2 0 00008
2 63010 42.9999 93.9944 0001584 255.6157 104.4535 15.70928019 05
| Epoch (UTC): | 25 May 2026 06:06:09 |
| Eccentricity: | 0.0001584 |
| inclination: | 42.9999° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 93.9944° |
| argument of perigee: | 255.6157° |
| revolutions per day: | 15.70928019 |
| mean anomaly at epoch: | 104.4535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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