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 64146U 26145.09599118 +.00000000 +00000-0 -48088-3 0 00006
2 64146 97.4514 196.4363 0001384 208.0989 152.0164 15.05634197 07
| Epoch (UTC): | 25 May 2026 02:18:13 |
| Eccentricity: | 0.0001384 |
| inclination: | 97.4514° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.4363° |
| argument of perigee: | 208.0989° |
| revolutions per day: | 15.05634197 |
| mean anomaly at epoch: | 152.0164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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