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 65275U 26145.10288135 +.00000000 +00000-0 -41980-4 0 00001
2 65275 97.4527 197.5353 0001474 157.2784 202.8509 15.05641694 01
| Epoch (UTC): | 25 May 2026 02:28:08 |
| Eccentricity: | 0.0001474 |
| inclination: | 97.4527° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 197.5353° |
| argument of perigee: | 157.2784° |
| revolutions per day: | 15.05641694 |
| mean anomaly at epoch: | 202.8509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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