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 64939U 26145.60212139 +.00000000 +00000-0 +36838-3 0 00007
2 64939 97.4499 9.5826 0002338 82.1151 278.0341 15.05660635 01
| Epoch (UTC): | 25 May 2026 14:27:03 |
| Eccentricity: | 0.0002338 |
| inclination: | 97.4499° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.5826° |
| argument of perigee: | 82.1151° |
| revolutions per day: | 15.05660635 |
| mean anomaly at epoch: | 278.0341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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