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 65840U 26145.25303076 +.00000000 +00000-0 +11504-2 0 00003
2 65840 53.1606 92.1470 0001145 74.4451 285.6678 15.34406562 03
| Epoch (UTC): | 25 May 2026 06:04:21 |
| Eccentricity: | 0.0001145 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.1470° |
| argument of perigee: | 74.4451° |
| revolutions per day: | 15.34406562 |
| mean anomaly at epoch: | 285.6678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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