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 63210U 26145.43244936 +.00000000 +00000-0 +51049-3 0 00000
2 63210 97.4031 42.1670 0004405 138.0517 222.1063 15.32683136 00
| Epoch (UTC): | 25 May 2026 10:22:43 |
| Eccentricity: | 0.0004405 |
| inclination: | 97.4031° |
| perigee height: | 465 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 42.1670° |
| argument of perigee: | 138.0517° |
| revolutions per day: | 15.32683136 |
| mean anomaly at epoch: | 222.1063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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