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 64840U 26145.32020215 +.00000000 +00000-0 +14751-3 0 00009
2 64840 97.7692 260.1047 0006736 63.9620 296.2293 14.94052790 06
| Epoch (UTC): | 25 May 2026 07:41:05 |
| Eccentricity: | 0.0006736 |
| inclination: | 97.7692° |
| perigee height: | 581 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 260.1047° |
| argument of perigee: | 63.9620° |
| revolutions per day: | 14.94052790 |
| mean anomaly at epoch: | 296.2293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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