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 64845U 26145.31630117 +.00000000 +00000-0 +14006-3 0 00004
2 64845 97.4500 0.5935 0002439 70.3693 289.7797 15.05654423 06
| Epoch (UTC): | 25 May 2026 07:35:28 |
| Eccentricity: | 0.0002439 |
| inclination: | 97.4500° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.5935° |
| argument of perigee: | 70.3693° |
| revolutions per day: | 15.05654423 |
| mean anomaly at epoch: | 289.7797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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