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 63241U 26145.21810424 +.00000000 +00000-0 +37496-3 0 00001
2 63241 97.3877 38.8968 0005184 228.8692 131.2100 15.27148349 08
| Epoch (UTC): | 25 May 2026 05:14:04 |
| Eccentricity: | 0.0005184 |
| inclination: | 97.3877° |
| perigee height: | 481 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 38.8968° |
| argument of perigee: | 228.8692° |
| revolutions per day: | 15.27148349 |
| mean anomaly at epoch: | 131.2100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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