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 63248U 26145.42588985 +.00000000 +00000-0 +37079-3 0 00002
2 63248 97.6911 38.2016 0001823 266.7683 93.3330 14.97557511 06
| Epoch (UTC): | 25 May 2026 10:13:16 |
| Eccentricity: | 0.0001823 |
| inclination: | 97.6911° |
| perigee height: | 573 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 38.2016° |
| argument of perigee: | 266.7683° |
| revolutions per day: | 14.97557511 |
| mean anomaly at epoch: | 93.3330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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