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 65828U 26145.54724235 +.00000000 +00000-0 +50561-3 0 00002
2 65828 53.1583 91.1354 0001544 85.3774 274.7405 15.34390646 07
| Epoch (UTC): | 25 May 2026 13:08:01 |
| Eccentricity: | 0.0001544 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 91.1354° |
| argument of perigee: | 85.3774° |
| revolutions per day: | 15.34390646 |
| mean anomaly at epoch: | 274.7405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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