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 64942U 26145.61042786 +.00000000 +00000-0 +19410-3 0 00008
2 64942 97.4496 9.5639 0002605 87.3737 272.7788 15.05656689 08
| Epoch (UTC): | 25 May 2026 14:39:00 |
| Eccentricity: | 0.0002605 |
| inclination: | 97.4496° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.5639° |
| argument of perigee: | 87.3737° |
| revolutions per day: | 15.05656689 |
| mean anomaly at epoch: | 272.7788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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