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 64854U 26145.33015755 +.00000000 +00000-0 +24646-3 0 00002
2 64854 97.4507 0.7320 0002746 82.1523 278.0016 15.05657003 09
| Epoch (UTC): | 25 May 2026 07:55:25 |
| Eccentricity: | 0.0002746 |
| inclination: | 97.4507° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.7320° |
| argument of perigee: | 82.1523° |
| revolutions per day: | 15.05657003 |
| mean anomaly at epoch: | 278.0016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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