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 65252U 26145.08155590 +.00000000 +00000-0 +20366-3 0 00004
2 65252 97.4485 187.9066 0001356 145.2163 214.9153 15.05651905 05
| Epoch (UTC): | 25 May 2026 01:57:26 |
| Eccentricity: | 0.0001356 |
| inclination: | 97.4485° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 187.9066° |
| argument of perigee: | 145.2163° |
| revolutions per day: | 15.05651905 |
| mean anomaly at epoch: | 214.9153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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