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 63240U 26145.43664103 +.00000000 +00000-0 +57879-3 0 00002
2 63240 97.3913 40.3196 0004980 212.3874 147.7062 15.30990908 01
| Epoch (UTC): | 25 May 2026 10:28:45 |
| Eccentricity: | 0.0004980 |
| inclination: | 97.3913° |
| perigee height: | 469 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.3196° |
| argument of perigee: | 212.3874° |
| revolutions per day: | 15.30990908 |
| mean anomaly at epoch: | 147.7062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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