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 65021U 26145.41886139 +.00000000 +00000-0 +27082-3 0 00007
2 65021 53.1604 298.0757 0001230 77.2899 282.8239 15.30222234 09
| Epoch (UTC): | 25 May 2026 10:03:09 |
| Eccentricity: | 0.0001230 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 298.0757° |
| argument of perigee: | 77.2899° |
| revolutions per day: | 15.30222234 |
| mean anomaly at epoch: | 282.8239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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