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 63250U 26145.64557962 +.00000000 +00000-0 +33418-3 0 00003
2 63250 97.6929 38.2307 0001507 266.5163 93.5887 14.97067988 04
| Epoch (UTC): | 25 May 2026 15:29:38 |
| Eccentricity: | 0.0001507 |
| inclination: | 97.6929° |
| perigee height: | 575 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 38.2307° |
| argument of perigee: | 266.5163° |
| revolutions per day: | 14.97067988 |
| mean anomaly at epoch: | 93.5887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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