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 64538U 26145.27712279 +.00000000 +00000-0 +17651-3 0 00007
2 64538 97.4675 260.1006 0003197 248.7405 111.3489 15.20164161 05
| Epoch (UTC): | 25 May 2026 06:39:03 |
| Eccentricity: | 0.0003197 |
| inclination: | 97.4675° |
| perigee height: | 503 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 260.1006° |
| argument of perigee: | 248.7405° |
| revolutions per day: | 15.20164161 |
| mean anomaly at epoch: | 111.3489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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