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 63216U 26145.42029064 +.00000000 +00000-0 +31696-3 0 00004
2 63216 97.3913 39.4953 0002302 153.2760 206.8598 15.26733438 06
| Epoch (UTC): | 25 May 2026 10:05:13 |
| Eccentricity: | 0.0002302 |
| inclination: | 97.3913° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 39.4953° |
| argument of perigee: | 153.2760° |
| revolutions per day: | 15.26733438 |
| mean anomaly at epoch: | 206.8598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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