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 64844U 26145.57105887 +.00000000 +00000-0 +19019-3 0 00001
2 64844 97.4510 0.8655 0002093 88.9766 271.1701 15.05656995 06
| Epoch (UTC): | 25 May 2026 13:42:19 |
| Eccentricity: | 0.0002093 |
| inclination: | 97.4510° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.8655° |
| argument of perigee: | 88.9766° |
| revolutions per day: | 15.05656995 |
| mean anomaly at epoch: | 271.1701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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