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 63296U 26145.62321244 +.00000000 +00000-0 +41956-3 0 00009
2 63296 97.6497 285.2091 0011645 197.1392 162.9448 15.16185100 08
| Epoch (UTC): | 25 May 2026 14:57:25 |
| Eccentricity: | 0.0011645 |
| inclination: | 97.6497° |
| perigee height: | 509 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 285.2091° |
| argument of perigee: | 197.1392° |
| revolutions per day: | 15.16185100 |
| mean anomaly at epoch: | 162.9448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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