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 63246U 26145.28088617 +.00000000 +00000-0 +66706-4 0 00001
2 63246 97.6858 37.6159 0003103 326.0480 34.0543 14.97236231 04
| Epoch (UTC): | 25 May 2026 06:44:28 |
| Eccentricity: | 0.0003103 |
| inclination: | 97.6858° |
| perigee height: | 573 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 37.6159° |
| argument of perigee: | 326.0480° |
| revolutions per day: | 14.97236231 |
| mean anomaly at epoch: | 34.0543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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