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 65328U 26145.39017095 +.00000000 +00000-0 +60511-3 0 00005
2 65328 53.1581 210.2186 0001026 37.1111 322.9961 15.31708022 03
| Epoch (UTC): | 25 May 2026 09:21:50 |
| Eccentricity: | 0.0001026 |
| inclination: | 53.1581° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 210.2186° |
| argument of perigee: | 37.1111° |
| revolutions per day: | 15.31708022 |
| mean anomaly at epoch: | 322.9961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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