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 65322U 26145.62900595 +.00000000 +00000-0 +14282-3 0 00005
2 65322 97.7371 221.2472 0011763 192.9495 167.1424 14.92704411 09
| Epoch (UTC): | 25 May 2026 15:05:46 |
| Eccentricity: | 0.0011763 |
| inclination: | 97.7371° |
| perigee height: | 581 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 221.2472° |
| argument of perigee: | 192.9495° |
| revolutions per day: | 14.92704411 |
| mean anomaly at epoch: | 167.1424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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